View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65596U 26145.14978793 +.00000000 +00000-0 +23719-3 0 00005
2 65596 97.4489 213.6185 0001737 176.8942 183.2297 15.05652072 00
| Epoch (UTC): | 25 May 2026 03:35:41 |
| Eccentricity: | 0.0001737 |
| inclination: | 97.4489° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.6185° |
| argument of perigee: | 176.8942° |
| revolutions per day: | 15.05652072 |
| mean anomaly at epoch: | 183.2297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|