| Mission type | Technology |
|---|---|
| Operator | University of Louisiana at Lafayette |
| COSPAR ID | 2013-064C |
| SATCAT no. | 39382 |
| Website | CAPE-2 |
| Mission duration | 11 months, 3 days |
| Spacecraft properties | |
| Spacecraft type | 1U CubeSat |
| Manufacturer | University of Louisiana at Lafayette |
| Launch mass | 1 kg (2.2 lb) |
| Dimensions | 10 cm × 10 cm × 10 cm (3.9 in × 3.9 in × 3.9 in) |
| Start of mission | |
| Launch date | 20 November 2013, 01:15 UTC[1] |
| Rocket | Minotaur I |
| Launch site | Wallops LA-0B[2] |
| Contractor | Northrop Grumman |
| End of mission | |
| Decay date | 23 October 2014 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 498 km (309 mi) |
| Apogee altitude | 500 km (310 mi) |
| Inclination | 40.51° |
| Period | 93.4 minutes |
| Epoch | 20 November 2013 |
CAPE-2 (Cajun Advanced Picosatellite Experiment 2), or Louisiana-OSCAR 75, was an American amateur miniaturized satellite developed by students at the University of Louisiana at Lafayette.[3]
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Report. Retrieved May 16, 2022.
- ^ Krebs, Gunter D. "CAPE 2 (Louisiana-OSCAR 75, LO 75)". Gunter's Space Page. Retrieved May 16, 2022.
- ^ "CAPE-2". University of Louisiana at Lafayette. 12 May 2017. Retrieved May 16, 2022.