MANDRAKE 2 ABLE is a payload in SSO orbit, operated by Space Development Agency / Defense Advanced Research Projects Agency, launched 2021.
| Orbit class | SSO |
| Inclination | 97.7037° |
| Eccentricity | 0.0003509 |
| Period | 92.6 min |
| Apogee | 402 km |
| Perigee | 397 km |
| Mean motion | 15.55818938 rev/day |
| RAAN | 19.2949° |
| Arg of perigee | 274.1422° |
| Mean anomaly | 85.9430° |
| B* | 2.4258e-4 |
| Rev at epoch | 28,020 |
1 48907U 21059AE 26187.98923791 .00016663 00000-0 24258-3 0 99932 48907 97.7037 19.2949 0003509 274.1422 85.9430 15.55818938280200{
"OBJECT_NAME": "MANDRAKE 2 ABLE",
"OBJECT_ID": "2021-059AE",
"EPOCH": "2026-07-06T23:44:30.155+00:00",
"MEAN_MOTION": 15.55818938,
"ECCENTRICITY": 0.0003509,
"INCLINATION": 97.7037,
"RA_OF_ASC_NODE": 19.2949,
"ARG_OF_PERICENTER": 274.1422,
"MEAN_ANOMALY": 85.943,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 48907,
"REV_AT_EPOCH": 28020,
"BSTAR": 0.00024258,
"MEAN_MOTION_DOT": 0.00016663,
"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 | MANDRAKE 2 ABLE |
| Operator | Space Development Agency / Defense Advanced Research Projects AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog |
| Country | United States |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |