View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62788U 26145.55061661 +.00000000 +00000-0 +13957-3 0 00000
2 62788 88.9709 86.0003 0011834 224.7002 135.3196 13.51012003 09
| Epoch (UTC): | 25 May 2026 13:12:53 |
| Eccentricity: | 0.0011834 |
| inclination: | 88.9709° |
| perigee height: | 1060 km |
| apogee height: | 1077 km |
| right ascension of ascending node: | 86.0003° |
| argument of perigee: | 224.7002° |
| revolutions per day: | 13.51012003 |
| mean anomaly at epoch: | 135.3196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|