View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61019U 26145.50229640 +.00000000 +00000-0 +17971-3 0 00004
2 61019 49.9964 187.9144 0022644 331.9664 28.0053 14.84156568 00
| Epoch (UTC): | 25 May 2026 12:03:18 |
| Eccentricity: | 0.0022644 |
| inclination: | 49.9964° |
| perigee height: | 600 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 187.9144° |
| argument of perigee: | 331.9664° |
| revolutions per day: | 14.84156568 |
| mean anomaly at epoch: | 28.0053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|