View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 23088U 94023B 25140.90404703 .00000318 00000-0 18912-3 0 9994
2 23088 70.9999 325.7370 0003032 345.8873 14.2165 14.14964480604672
| Epoch (UTC): | 20 May 2025 21:41:49 |
| Eccentricity: | 0.0003032 |
| inclination: | 70.9999° |
| perigee height: | 840 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 325.7370° |
| argument of perigee: | 345.8873° |
| revolutions per day: | 14.14964480 |
| mean anomaly at epoch: | 14.2165° |
| orbit number at epoch: | 60467 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|