View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64935U 26145.55229568 +.00000000 +00000-0 +31099-3 0 00005
2 64935 97.4484 9.4942 0002558 91.6545 268.4975 15.05655467 08
| Epoch (UTC): | 25 May 2026 13:15:18 |
| Eccentricity: | 0.0002558 |
| inclination: | 97.4484° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.4942° |
| argument of perigee: | 91.6545° |
| revolutions per day: | 15.05655467 |
| mean anomaly at epoch: | 268.4975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|