TOMORROW-R2 is a payload in SSO orbit, operated by Tomorrow.io (The Tomorrow Companies Inc.), launched 2023.
Orbital data last updated 10 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | SSO |
| Inclination | 97.5927° |
| Eccentricity | 0.0016127 |
| Period | 87.7 min |
| Apogee | 170 km |
| Perigee | 149 km |
| Mean motion | 16.42499341 rev/day |
| RAAN | 344.0780° |
| Arg of perigee | 249.9450° |
| Mean anomaly | 110.0115° |
| B* | 2.9152e-4 |
| Rev at epoch | 17,067 |
This object is recorded as DECAYED (re-entered). These are the last known elements before re-entry — not a current orbit.
1 56962U 23084AG 26178.18999233 .07878607 26806-5 29152-3 0 99952 56962 97.5927 344.0780 0016127 249.9450 110.0115 16.42499341170678{
"OBJECT_NAME": "TOMORROW-R2",
"OBJECT_ID": "2023-084AG",
"EPOCH": "2026-06-27T04:33:35.337+00:00",
"MEAN_MOTION": 16.42499341,
"ECCENTRICITY": 0.0016127,
"INCLINATION": 97.5927,
"RA_OF_ASC_NODE": 344.078,
"ARG_OF_PERICENTER": 249.945,
"MEAN_ANOMALY": 110.0115,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 56962,
"REV_AT_EPOCH": 17067,
"BSTAR": 0.00029152,
"MEAN_MOTION_DOT": 0.07878607,
"MEAN_MOTION_DDOT": 0.0000026806
}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 | TOMORROW-R2 |
| 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 |
| Decay date |