MANDRAKE 2 BAKER is a payload in SSO orbit, operated by Space Development Agency / Defense Advanced Research Projects Agency, launched 2021.
| Orbit class | SSO |
| Inclination | 97.7000° |
| Eccentricity | 0.0002198 |
| Period | 92.3 min |
| Apogee | 387 km |
| Perigee | 384 km |
| Mean motion | 15.60598515 rev/day |
| RAAN | 21.3340° |
| Arg of perigee | 267.2089° |
| Mean anomaly | 92.8916° |
| B* | 3.7921e-4 |
| Rev at epoch | 28,024 |
1 48908U 21059AF 26187.09201249 .00031291 00000-0 37921-3 0 99982 48908 97.7000 21.3340 0002198 267.2089 92.8916 15.60598515280247{
"OBJECT_NAME": "MANDRAKE 2 BAKER",
"OBJECT_ID": "2021-059AF",
"EPOCH": "2026-07-06T02:12:29.879+00:00",
"MEAN_MOTION": 15.60598515,
"ECCENTRICITY": 0.0002198,
"INCLINATION": 97.7,
"RA_OF_ASC_NODE": 21.334,
"ARG_OF_PERICENTER": 267.2089,
"MEAN_ANOMALY": 92.8916,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 48908,
"REV_AT_EPOCH": 28024,
"BSTAR": 0.00037921,
"MEAN_MOTION_DOT": 0.00031291,
"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 BAKER |
| 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 |