View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62488U 26145.24233566 +.00000000 +00000-0 +59540-3 0 00006
2 62488 42.9959 216.2714 0000678 293.6458 66.4323 15.27588861 04
| Epoch (UTC): | 25 May 2026 05:48:57 |
| Eccentricity: | 0.0000678 |
| inclination: | 42.9959° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 216.2714° |
| argument of perigee: | 293.6458° |
| revolutions per day: | 15.27588861 |
| mean anomaly at epoch: | 66.4323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|