View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 41915U 17002C 25307.01955990 .09824273 25211-5 80465-3 0 9992
2 41915 97.1100 340.3214 0005056 183.3807 176.7459 16.39937900489044
| Epoch (UTC): | 03 November 2025 00:28:09 |
| Eccentricity: | 0.0005056 |
| inclination: | 97.1100° |
| perigee height: | 162 km |
| apogee height: | 169 km |
| right ascension of ascending node: | 340.3214° |
| argument of perigee: | 183.3807° |
| revolutions per day: | 16.39937900 |
| mean anomaly at epoch: | 176.7459° |
| orbit number at epoch: | 48904 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|