View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63037U 26145.58335647 +.00000000 +00000-0 -12219-3 0 00000
2 63037 53.1587 261.0868 0001485 89.0022 62.7722 15.33562086 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001485 |
| inclination: | 53.1587° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 261.0868° |
| argument of perigee: | 89.0022° |
| revolutions per day: | 15.33562086 |
| mean anomaly at epoch: | 62.7722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|