View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65072U 26145.46052605 +.00000000 +00000-0 +25786-3 0 00000
2 65072 97.4467 222.5482 0002301 147.4719 212.6650 15.05654639 09
| Epoch (UTC): | 25 May 2026 11:03:09 |
| Eccentricity: | 0.0002301 |
| inclination: | 97.4467° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.5482° |
| argument of perigee: | 147.4719° |
| revolutions per day: | 15.05654639 |
| mean anomaly at epoch: | 212.6650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|