View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52461U 26145.04808861 +.00000000 +00000-0 +23049-4 0 00006
2 52461 53.2167 66.3348 0001117 85.5639 274.5481 15.08836007 09
| Epoch (UTC): | 25 May 2026 01:09:14 |
| Eccentricity: | 0.0001117 |
| inclination: | 53.2167° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 66.3348° |
| argument of perigee: | 85.5639° |
| revolutions per day: | 15.08836007 |
| mean anomaly at epoch: | 274.5481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|