View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 35869U 09049E 25194.14440286 .00000040 00000-0 37068-4 0 9995
2 35869 98.6879 154.3619 0004036 189.7477 170.3624 14.23098127821286
| Epoch (UTC): | 13 July 2025 03:27:56 |
| Eccentricity: | 0.0004036 |
| inclination: | 98.6879° |
| perigee height: | 812 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 154.3619° |
| argument of perigee: | 189.7477° |
| revolutions per day: | 14.23098127 |
| mean anomaly at epoch: | 170.3624° |
| orbit number at epoch: | 82128 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|