View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 30015U 99025MQ 24276.87704258 .00012958 00000-0 51911-2 0 9990
2 30015 99.1965 248.5148 0039007 303.5095 85.3866 14.28000278919452
| Epoch (UTC): | 02 October 2024 21:02:56 |
| Eccentricity: | 0.0039007 |
| inclination: | 99.1965° |
| perigee height: | 770 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 248.5148° |
| argument of perigee: | 303.5095° |
| revolutions per day: | 14.28000278 |
| mean anomaly at epoch: | 85.3866° |
| orbit number at epoch: | 91945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|