View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49153U 26145.20790147 +.00000000 +00000-0 +42825-4 0 00008
2 49153 70.0005 61.5264 0002895 269.2337 90.8491 14.98332538 03
| Epoch (UTC): | 25 May 2026 04:59:22 |
| Eccentricity: | 0.0002895 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 61.5264° |
| argument of perigee: | 269.2337° |
| revolutions per day: | 14.98332538 |
| mean anomaly at epoch: | 90.8491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|