View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54644U 26145.35501883 +.00000000 +00000-0 -17111-4 0 00003
2 54644 87.9259 248.5128 0002131 95.5393 264.5984 13.21825461 07
| Epoch (UTC): | 25 May 2026 08:31:13 |
| Eccentricity: | 0.0002131 |
| inclination: | 87.9259° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.5128° |
| argument of perigee: | 95.5393° |
| revolutions per day: | 13.21825461 |
| mean anomaly at epoch: | 264.5984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|