View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60275U 26145.05470007 +.00000000 +00000-0 +96774-5 0 00002
2 60275 53.1605 57.4926 0001108 94.4420 265.6707 15.30192180 01
| Epoch (UTC): | 25 May 2026 01:18:46 |
| Eccentricity: | 0.0001108 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.4926° |
| argument of perigee: | 94.4420° |
| revolutions per day: | 15.30192180 |
| mean anomaly at epoch: | 265.6707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|