View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 06920U 26121.97545852 +.00000000 +00000-0 +64811-4 0 00001
2 06920 102.2862 135.4703 0006326 207.2661 180.2582 12.40393116 00
| Epoch (UTC): | 01 May 2026 23:24:39 |
| Eccentricity: | 0.0006326 |
| inclination: | 102.2862° |
| perigee height: | 1500 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 135.4703° |
| argument of perigee: | 207.2661° |
| revolutions per day: | 12.40393116 |
| mean anomaly at epoch: | 180.2582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|