View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66096U 26145.60160434 +.00000000 +00000-0 +57646-3 0 00003
2 66096 53.1594 106.3721 0001342 92.5467 267.5688 15.30193640 03
| Epoch (UTC): | 25 May 2026 14:26:18 |
| Eccentricity: | 0.0001342 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.3721° |
| argument of perigee: | 92.5467° |
| revolutions per day: | 15.30193640 |
| mean anomaly at epoch: | 267.5688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|