ABS-3A is a payload in GEO orbit, operated by ABS Global Satellite Ltd., launched 2015.
| Orbit class | GEO |
| Inclination | 0.0440° |
| Eccentricity | 0.0001587 |
| Period | 1436.1 min |
| Apogee | 35,794 km |
| Perigee | 35,781 km |
| Mean motion | 1.00268909 rev/day |
| RAAN | 66.3870° |
| Arg of perigee | 348.5463° |
| Mean anomaly | 290.8882° |
| B* | 0.0000e+0 |
| Rev at epoch | 4,157 |
1 40424U 15010A 26188.17683735 .00000000 00000-0 00000-0 0 99962 40424 0.0440 66.3870 0001587 348.5463 290.8882 1.00268909 41577{
"OBJECT_NAME": "ABS-3A",
"OBJECT_ID": "2015-010A",
"EPOCH": "2026-07-07T04:14:38.747+00:00",
"MEAN_MOTION": 1.00268909,
"ECCENTRICITY": 0.0001587,
"INCLINATION": 0.044,
"RA_OF_ASC_NODE": 66.387,
"ARG_OF_PERICENTER": 348.5463,
"MEAN_ANOMALY": 290.8882,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 40424,
"REV_AT_EPOCH": 4157,
"BSTAR": 0,
"MEAN_MOTION_DOT": 0,
"MEAN_MOTION_DDOT": 0
}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 | ABS-3A |
| Operator | |
| Country | PG |
| Launch date | |
| Launch mass (kg) | |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose |
| — |
| Object class |
| Orbital regime |
| Status |