View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31702U 26041.92002993 +.00000000 +00000-0 +73985-3 0 00008
2 31702 63.3104 261.5164 0500532 41.8504 321.9727 14.50768936 04
| Epoch (UTC): | 10 February 2026 22:04:50 |
| Eccentricity: | 0.0500532 |
| inclination: | 63.3104° |
| perigee height: | 368 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 261.5164° |
| argument of perigee: | 41.8504° |
| revolutions per day: | 14.50768936 |
| mean anomaly at epoch: | 321.9727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|