View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45453U 26145.51468757 +.00000000 +00000-0 +13964-3 0 00001
2 45453 88.9303 236.2873 0005814 74.7776 285.4096 14.90258833 08
| Epoch (UTC): | 25 May 2026 12:21:09 |
| Eccentricity: | 0.0005814 |
| inclination: | 88.9303° |
| perigee height: | 593 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 236.2873° |
| argument of perigee: | 74.7776° |
| revolutions per day: | 14.90258833 |
| mean anomaly at epoch: | 285.4096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|