LEMUR-2-OBA-NI-JESU is a payload in SSO orbit, operated by Spire / NorthStar Earth and Space, launched 2024.
Orbital data last updated 25 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | SSO |
| Inclination | 97.3656° |
| Eccentricity | 0.0007133 |
| Period | 88.7 min |
| Apogee | 213 km |
| Perigee | 204 km |
| Mean motion | 16.24065045 rev/day |
| RAAN | 28.2035° |
| Arg of perigee | 233.9694° |
| Mean anomaly | 126.0937° |
| B* | 1.2613e-3 |
| Rev at epoch | 13,252 |
1 58902U 24022D 26163.08060411 .03279838 24474-5 12613-2 0 99932 58902 97.3656 28.2035 0007133 233.9694 126.0937 16.24065045132526{
"OBJECT_NAME": "LEMUR-2-OBA-NI-JESU",
"OBJECT_ID": "2024-022D",
"EPOCH": "2026-06-12T01:56:04.195+00:00",
"MEAN_MOTION": 16.24065045,
"ECCENTRICITY": 0.00071325,
"INCLINATION": 97.3656,
"RA_OF_ASC_NODE": 28.2035,
"ARG_OF_PERICENTER": 233.9694,
"MEAN_ANOMALY": 126.0937,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 58902,
"REV_AT_EPOCH": 13252,
"BSTAR": 0.0012613048,
"MEAN_MOTION_DOT": 0.03279838,
"MEAN_MOTION_DDOT": 0.000002447398
}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 | LEMUR-2-OBA-NI-JESU |
| Operator | |
| 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 |