POPACS 2 is a payload in VLEO orbit, operated by Project POPACS (Gil Moore), launched 2013.
| Orbit class | VLEO |
| Inclination | 80.9915° |
| Eccentricity | 0.0415832 |
| Period | 96.5 min |
| Apogee | 882 km |
| Perigee | 303 km |
| Mean motion | 14.91720341 rev/day |
| RAAN | 124.0034° |
| Arg of perigee | 137.1605° |
| Mean anomaly | 226.2823° |
| B* | 4.4971e-4 |
| Rev at epoch | 66,584 |
1 39269U 13055E 26185.82184007 .00027129 -75250-6 44971-3 0 99902 39269 80.9915 124.0034 0415832 137.1605 226.2823 14.91720341665849{
"OBJECT_NAME": "POPACS 2",
"OBJECT_ID": "2013-055E",
"EPOCH": "2026-07-04T19:43:26.982+00:00",
"MEAN_MOTION": 14.91720341,
"ECCENTRICITY": 0.0415832,
"INCLINATION": 80.9915,
"RA_OF_ASC_NODE": 124.0034,
"ARG_OF_PERICENTER": 137.1605,
"MEAN_ANOMALY": 226.2823,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 39269,
"REV_AT_EPOCH": 66584,
"BSTAR": 0.00044970881,
"MEAN_MOTION_DOT": 0.00027129,
"MEAN_MOTION_DDOT": -7.52503e-7
}Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.
| Name | POPACS 2 |
| Operator | |
| Country | United States |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |