View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53435U 26145.24356626 +.00000000 +00000-0 +14521-3 0 00001
2 53435 53.2144 120.2579 0001332 88.5312 271.5833 15.08833508 03
| Epoch (UTC): | 25 May 2026 05:50:44 |
| Eccentricity: | 0.0001332 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 120.2579° |
| argument of perigee: | 88.5312° |
| revolutions per day: | 15.08833508 |
| mean anomaly at epoch: | 271.5833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|