LEMUR-2-EMBRIONOVIS is a payload in SSO orbit, operated by Spire / Orora Technologies GmbH, launched 2023.
| Orbit class | SSO |
| Inclination | 97.6318° |
| Eccentricity | 0.0007739 |
| Period | 93.6 min |
| Apogee | 457 km |
| Perigee | 447 km |
| Mean motion | 15.38076097 rev/day |
| RAAN | 332.8842° |
| Arg of perigee | 238.8204° |
| Mean anomaly | 121.2282° |
| B* | 2.8396e-4 |
| Rev at epoch | 17,071 |
1 56970U 23084AQ 26187.91800207 .00010566 00000-0 28396-3 0 99942 56970 97.6318 332.8842 0007739 238.8204 121.2282 15.38076097170716{
"OBJECT_NAME": "LEMUR-2-EMBRIONOVIS",
"OBJECT_ID": "2023-084AQ",
"EPOCH": "2026-07-06T22:01:55.379+00:00",
"MEAN_MOTION": 15.38076097,
"ECCENTRICITY": 0.0007739,
"INCLINATION": 97.6318,
"RA_OF_ASC_NODE": 332.8842,
"ARG_OF_PERICENTER": 238.8204,
"MEAN_ANOMALY": 121.2282,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 56970,
"REV_AT_EPOCH": 17071,
"BSTAR": 0.00028396,
"MEAN_MOTION_DOT": 0.00010566,
"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 | LEMUR-2-EMBRIONOVIS |
| 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 |