View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45693U 26145.48270956 +.00000000 +00000-0 +11489-2 0 00004
2 45693 53.0502 65.2506 0006094 93.5657 266.6033 15.16038152 00
| Epoch (UTC): | 25 May 2026 11:35:06 |
| Eccentricity: | 0.0006094 |
| inclination: | 53.0502° |
| perigee height: | 514 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 65.2506° |
| argument of perigee: | 93.5657° |
| revolutions per day: | 15.16038152 |
| mean anomaly at epoch: | 266.6033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|