View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23410U 26088.07146959 +.00000000 +00000-0 +98851-4 0 00003
2 23410 70.9797 322.9359 0223098 244.4574 268.2341 13.68697553 07
| Epoch (UTC): | 29 March 2026 01:42:54 |
| Eccentricity: | 0.0223098 |
| inclination: | 70.9797° |
| perigee height: | 840 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 322.9359° |
| argument of perigee: | 244.4574° |
| revolutions per day: | 13.68697553 |
| mean anomaly at epoch: | 268.2341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|