View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64877U 26145.61549041 +.00000000 +00000-0 +38375-4 0 00003
2 64877 98.6013 108.0083 0000534 77.3783 282.7454 14.21484073 04
| Epoch (UTC): | 25 May 2026 14:46:18 |
| Eccentricity: | 0.0000534 |
| inclination: | 98.6013° |
| perigee height: | 820 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 108.0083° |
| argument of perigee: | 77.3783° |
| revolutions per day: | 14.21484073 |
| mean anomaly at epoch: | 282.7454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|