View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68587U 26145.11728133 +.00000000 +00000-0 +81987-3 0 00007
2 68587 51.8730 288.3137 0004316 280.4929 79.5572 15.38493093 00
| Epoch (UTC): | 25 May 2026 02:48:53 |
| Eccentricity: | 0.0004316 |
| inclination: | 51.8730° |
| perigee height: | 448 km |
| apogee height: | 454 km |
| right ascension of ascending node: | 288.3137° |
| argument of perigee: | 280.4929° |
| revolutions per day: | 15.38493093 |
| mean anomaly at epoch: | 79.5572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|