View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49164U 26145.54611200 +.00000000 +00000-0 +22200-4 0 00004
2 49164 70.0003 80.6721 0002705 267.2381 92.8468 14.98330160 05
| Epoch (UTC): | 25 May 2026 13:06:24 |
| Eccentricity: | 0.0002705 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.6721° |
| argument of perigee: | 267.2381° |
| revolutions per day: | 14.98330160 |
| mean anomaly at epoch: | 92.8468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|