View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61881U 26144.95937081 +.00000000 +00000-0 +68660-5 0 00007
2 61881 53.1579 340.2778 0000893 52.4084 307.7015 15.69707540 07
| Epoch (UTC): | 24 May 2026 23:01:29 |
| Eccentricity: | 0.0000893 |
| inclination: | 53.1579° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 340.2778° |
| argument of perigee: | 52.4084° |
| revolutions per day: | 15.69707540 |
| mean anomaly at epoch: | 307.7015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|