View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65792U 26145.40415632 +.00000000 +00000-0 +31396-3 0 00000
2 65792 97.4491 8.1948 0002600 77.7500 282.4018 15.05658642 06
| Epoch (UTC): | 25 May 2026 09:41:59 |
| Eccentricity: | 0.0002600 |
| inclination: | 97.4491° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.1948° |
| argument of perigee: | 77.7500° |
| revolutions per day: | 15.05658642 |
| mean anomaly at epoch: | 282.4018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|