View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 12508U 26088.02629212 +.00000000 +00000-0 +72772-4 0 00006
2 12508 82.9546 287.1883 0036308 235.1055 124.6688 13.76636480 09
| Epoch (UTC): | 29 March 2026 00:37:51 |
| Eccentricity: | 0.0036308 |
| inclination: | 82.9546° |
| perigee height: | 949 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 287.1883° |
| argument of perigee: | 235.1055° |
| revolutions per day: | 13.76636480 |
| mean anomaly at epoch: | 124.6688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|