View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63096U 26145.43856926 +.00000000 +00000-0 +39685-3 0 00002
2 63096 70.0004 161.1278 0002796 257.7563 102.3283 14.98348282 00
| Epoch (UTC): | 25 May 2026 10:31:32 |
| Eccentricity: | 0.0002796 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 161.1278° |
| argument of perigee: | 257.7563° |
| revolutions per day: | 14.98348282 |
| mean anomaly at epoch: | 102.3283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|