View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00116U 61015A 23150.34532986 .00000063 00000-0 10683-3 0 9992
2 00116 66.8096 95.4336 0079188 329.5088 30.1398 13.91918078141662
| Epoch (UTC): | 30 May 2023 08:17:16 |
| Eccentricity: | 0.0079188 |
| inclination: | 66.8096° |
| perigee height: | 864 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 95.4336° |
| argument of perigee: | 329.5088° |
| revolutions per day: | 13.91918078 |
| mean anomaly at epoch: | 30.1398° |
| orbit number at epoch: | 14166 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|