View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22627U 26157.13972205 +.00000000 +00000-0 +51969-4 0 00006
2 22627 82.5212 295.3630 0023821 53.5272 306.8132 14.80151936 00
| Epoch (UTC): | 06 June 2026 03:21:11 |
| Eccentricity: | 0.0023821 |
| inclination: | 82.5212° |
| perigee height: | 612 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 295.3630° |
| argument of perigee: | 53.5272° |
| revolutions per day: | 14.80151936 |
| mean anomaly at epoch: | 306.8132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|