View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45689U 26145.45850755 +.00000000 +00000-0 +12197-2 0 00004
2 45689 53.1584 52.4048 0003101 113.4200 246.7128 15.33646333 06
| Epoch (UTC): | 25 May 2026 11:00:15 |
| Eccentricity: | 0.0003101 |
| inclination: | 53.1584° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 52.4048° |
| argument of perigee: | 113.4200° |
| revolutions per day: | 15.33646333 |
| mean anomaly at epoch: | 246.7128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|