View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54130U 26145.18419822 +.00000000 +00000-0 +13448-3 0 00002
2 54130 87.9150 309.5587 0001789 82.4022 277.7313 13.19727080 03
| Epoch (UTC): | 25 May 2026 04:25:14 |
| Eccentricity: | 0.0001789 |
| inclination: | 87.9150° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5587° |
| argument of perigee: | 82.4022° |
| revolutions per day: | 13.19727080 |
| mean anomaly at epoch: | 277.7313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|