View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61220U 26145.50963309 +.00000000 +00000-0 +27775-3 0 00008
2 61220 98.0424 235.6481 0001420 161.1339 198.9921 14.72303048 01
| Epoch (UTC): | 25 May 2026 12:13:52 |
| Eccentricity: | 0.0001420 |
| inclination: | 98.0424° |
| perigee height: | 653 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 235.6481° |
| argument of perigee: | 161.1339° |
| revolutions per day: | 14.72303048 |
| mean anomaly at epoch: | 198.9921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|