SPEQTRE is a payload in SSO orbit, operated by Rutherford Appleton Laboratory / SpeQtral, launched 2025.
| Orbit class | SSO |
| Inclination | 97.4196° |
| Eccentricity | 0.0002489 |
| Period | 94.7 min |
| Apogee | 506 km |
| Perigee | 502 km |
| Mean motion | 15.20677224 rev/day |
| RAAN | 261.6733° |
| Arg of perigee | 124.7761° |
| Mean anomaly | 235.3709° |
| B* | 1.6343e-4 |
| Rev at epoch | 3,347 |
1 66769U 25276DH 26188.16497235 .00003521 00000-0 16343-3 0 99992 66769 97.4196 261.6733 0002489 124.7761 235.3709 15.20677224 33473{
"OBJECT_NAME": "SPEQTRE",
"OBJECT_ID": "2025-276DH",
"EPOCH": "2026-07-07T03:57:33.611+00:00",
"MEAN_MOTION": 15.20677224,
"ECCENTRICITY": 0.0002489,
"INCLINATION": 97.4196,
"RA_OF_ASC_NODE": 261.6733,
"ARG_OF_PERICENTER": 124.7761,
"MEAN_ANOMALY": 235.3709,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 66769,
"REV_AT_EPOCH": 3347,
"BSTAR": 0.00016343,
"MEAN_MOTION_DOT": 0.00003521,
"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 | SPEQTRE |
| Operator | |
| Country | United Kingdom |
| 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 |