View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53038U 26145.24634510 +.00000000 +00000-0 +12605-4 0 00003
2 53038 53.2137 90.4426 0001082 86.1671 273.9445 15.08843121 04
| Epoch (UTC): | 25 May 2026 05:54:44 |
| Eccentricity: | 0.0001082 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 90.4426° |
| argument of perigee: | 86.1671° |
| revolutions per day: | 15.08843121 |
| mean anomaly at epoch: | 273.9445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|