LEMUR-2-MANO is a payload in SSO orbit, operated by Spire, launched 2023.
Orbital data last updated 46 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | SSO |
| Inclination | 99.4457° |
| Eccentricity | 0.0026498 |
| Period | 89.4 min |
| Apogee | 264 km |
| Perigee | 229 km |
| Mean motion | 16.10055558 rev/day |
| RAAN | 191.1673° |
| Arg of perigee | 201.8616° |
| Mean anomaly | 158.1532° |
| B* | 1.2752e-3 |
| Rev at epoch | 15,804 |
1 57390U 23100E 26141.96203777 .01234281 98047-3 12752-2 0 99962 57390 99.4457 191.1673 0026498 201.8616 158.1532 16.10055558158044{
"OBJECT_NAME": "LEMUR-2-MANO",
"OBJECT_ID": "2023-100E",
"EPOCH": "2026-05-21T23:05:20.063+00:00",
"MEAN_MOTION": 16.10055558,
"ECCENTRICITY": 0.00264978,
"INCLINATION": 99.4457,
"RA_OF_ASC_NODE": 191.1673,
"ARG_OF_PERICENTER": 201.8616,
"MEAN_ANOMALY": 158.1532,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 57390,
"REV_AT_EPOCH": 15804,
"BSTAR": 0.0012751706,
"MEAN_MOTION_DOT": 0.01234281,
"MEAN_MOTION_DDOT": 0.0009804687
}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-MANO |
| 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 |