View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53283U 26145.44230617 +.00000000 +00000-0 +33318-4 0 00001
2 53283 53.2117 199.5644 0001153 72.5453 287.5666 15.08836599 00
| Epoch (UTC): | 25 May 2026 10:36:55 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 199.5644° |
| argument of perigee: | 72.5453° |
| revolutions per day: | 15.08836599 |
| mean anomaly at epoch: | 287.5666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|