View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 01814U 26088.20762330 +.00000000 +00000-0 +15902-3 0 00004
2 01814 75.8640 129.0258 0006289 297.4822 62.5720 14.71548914 08
| Epoch (UTC): | 29 March 2026 04:58:58 |
| Eccentricity: | 0.0006289 |
| inclination: | 75.8640° |
| perigee height: | 652 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 129.0258° |
| argument of perigee: | 297.4822° |
| revolutions per day: | 14.71548914 |
| mean anomaly at epoch: | 62.5720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|