View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55958U 26145.20175934 +.00000000 +00000-0 -16410-3 0 00000
2 55958 70.0005 71.5580 0003084 274.9217 85.1590 14.98329810 02
| Epoch (UTC): | 25 May 2026 04:50:32 |
| Eccentricity: | 0.0003084 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 71.5580° |
| argument of perigee: | 274.9217° |
| revolutions per day: | 14.98329810 |
| mean anomaly at epoch: | 85.1590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|