LEMUR-2-PEGGY-2004 is a payload in SSO orbit, operated by Spire, launched 2026.
| Orbit class | SSO |
| Inclination | 97.7555° |
| Eccentricity | 0.0002077 |
| Period | 96.5 min |
| Apogee | 590 km |
| Perigee | 587 km |
| Mean motion | 14.92941055 rev/day |
| RAAN | 145.4558° |
| Arg of perigee | 125.4827° |
| Mean anomaly | 234.6587° |
| B* | 3.3327e-4 |
| Rev at epoch | 1,460 |
1 68479U 26067BR 26187.45640146 .00003403 00000-0 33327-3 0 99902 68479 97.7555 145.4558 0002077 125.4827 234.6587 14.92941055 14607{
"OBJECT_NAME": "LEMUR-2-PEGGY-2004",
"OBJECT_ID": "2026-067BR",
"EPOCH": "2026-07-06T10:57:13.086+00:00",
"MEAN_MOTION": 14.92941055,
"ECCENTRICITY": 0.0002077,
"INCLINATION": 97.7555,
"RA_OF_ASC_NODE": 145.4558,
"ARG_OF_PERICENTER": 125.4827,
"MEAN_ANOMALY": 234.6587,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 68479,
"REV_AT_EPOCH": 1460,
"BSTAR": 0.00033327,
"MEAN_MOTION_DOT": 0.00003403,
"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-PEGGY-2004 |
| 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 |