View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41457U 26152.00077417 +.00000000 +00000-0 +22783-3 0 00001
2 41457 98.2441 164.7590 0001035 101.4188 258.7128 14.59558409 08
| Epoch (UTC): | 01 June 2026 00:01:06 |
| Eccentricity: | 0.0001035 |
| inclination: | 98.2441° |
| perigee height: | 694 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 164.7590° |
| argument of perigee: | 101.4188° |
| revolutions per day: | 14.59558409 |
| mean anomaly at epoch: | 258.7128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|