View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62138U 26145.59448453 +.00000000 +00000-0 +16468-3 0 00001
2 62138 97.4384 349.3617 0001702 93.0297 267.1133 15.19758489 00
| Epoch (UTC): | 25 May 2026 14:16:03 |
| Eccentricity: | 0.0001702 |
| inclination: | 97.4384° |
| perigee height: | 505 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 349.3617° |
| argument of perigee: | 93.0297° |
| revolutions per day: | 15.19758489 |
| mean anomaly at epoch: | 267.1133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|