View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25544U 26068.70691881 +.00000000 +00000-0 +15510-3 0 00000
2 25544 51.6323 72.2710 0008020 174.6781 185.4294 15.48547200 04
| Epoch (UTC): | 09 March 2026 16:57:57 |
| Eccentricity: | 0.0008020 |
| inclination: | 51.6323° |
| perigee height: | 416 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 72.2710° |
| argument of perigee: | 174.6781° |
| revolutions per day: | 15.48547200 |
| mean anomaly at epoch: | 185.4294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|