View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25261U 26037.60617825 +.00000000 +00000-0 +19863-3 0 00002
2 25261 98.8297 65.4405 0004126 138.6963 221.4534 14.36239069 08
| Epoch (UTC): | 06 February 2026 14:32:53 |
| Eccentricity: | 0.0004126 |
| inclination: | 98.8297° |
| perigee height: | 768 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 65.4405° |
| argument of perigee: | 138.6963° |
| revolutions per day: | 14.36239069 |
| mean anomaly at epoch: | 221.4534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|