View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40045U 26145.37892601 +.00000000 +00000-0 +45270-3 0 00001
2 40045 97.7211 312.5788 0039556 91.9424 268.6329 14.97811481 03
| Epoch (UTC): | 25 May 2026 09:05:39 |
| Eccentricity: | 0.0039556 |
| inclination: | 97.7211° |
| perigee height: | 546 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 312.5788° |
| argument of perigee: | 91.9424° |
| revolutions per day: | 14.97811481 |
| mean anomaly at epoch: | 268.6329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|