View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53138U 26145.50810688 +.00000000 +00000-0 +67522-5 0 00004
2 53138 53.2118 184.4525 0000980 93.7768 266.3336 15.08843336 08
| Epoch (UTC): | 25 May 2026 12:11:40 |
| Eccentricity: | 0.0000980 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 184.4525° |
| argument of perigee: | 93.7768° |
| revolutions per day: | 15.08843336 |
| mean anomaly at epoch: | 266.3336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|