View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39420U 26141.09339470 +.00000000 +00000-0 +13498-3 0 00008
2 39420 97.6840 7.4324 0118193 98.7441 262.7175 14.72245427 08
| Epoch (UTC): | 21 May 2026 02:14:29 |
| Eccentricity: | 0.0118193 |
| inclination: | 97.6840° |
| perigee height: | 571 km |
| apogee height: | 737 km |
| right ascension of ascending node: | 7.4324° |
| argument of perigee: | 98.7441° |
| revolutions per day: | 14.72245427 |
| mean anomaly at epoch: | 262.7175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|