R2 is a payload in LEO orbit, operated by NanoAvionics, launched 2020.
| Orbit class | LEO |
| Inclination | 36.8978° |
| Eccentricity | 0.0006870 |
| Period | 94.4 min |
| Apogee | 493 km |
| Perigee | 484 km |
| Mean motion | 15.25733870 rev/day |
| RAAN | 303.1680° |
| Arg of perigee | 85.0008° |
| Mean anomaly | 275.1525° |
| B* | 3.1212e-4 |
| Rev at epoch | 31,491 |
1 46913U 20081J 26187.36083685 .00008064 00000-0 31212-3 0 99972 46913 36.8978 303.1680 0006870 85.0008 275.1525 15.25733870314915{
"OBJECT_NAME": "R2",
"OBJECT_ID": "2020-081J",
"EPOCH": "2026-07-06T08:39:36.304+00:00",
"MEAN_MOTION": 15.2573387,
"ECCENTRICITY": 0.00068702,
"INCLINATION": 36.8978,
"RA_OF_ASC_NODE": 303.168,
"ARG_OF_PERICENTER": 85.0008,
"MEAN_ANOMALY": 275.1525,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 46913,
"REV_AT_EPOCH": 31491,
"BSTAR": 0.00031211581,
"MEAN_MOTION_DOT": 0.00008064,
"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 | R2 |
| Operator | |
| Country | |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |