View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55774U 26145.39322802 +.00000000 +00000-0 -10567-3 0 00001
2 55774 70.0005 31.0172 0002722 272.7546 87.3302 14.98338695 01
| Epoch (UTC): | 25 May 2026 09:26:14 |
| Eccentricity: | 0.0002722 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.0172° |
| argument of perigee: | 272.7546° |
| revolutions per day: | 14.98338695 |
| mean anomaly at epoch: | 87.3302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|