View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40030U 26145.44927708 +.00000000 +00000-0 +36428-3 0 00005
2 40030 98.0868 141.7394 0006624 323.8038 36.2743 15.14673921 06
| Epoch (UTC): | 25 May 2026 10:46:57 |
| Eccentricity: | 0.0006624 |
| inclination: | 98.0868° |
| perigee height: | 517 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 141.7394° |
| argument of perigee: | 323.8038° |
| revolutions per day: | 15.14673921 |
| mean anomaly at epoch: | 36.2743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|