View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27619U 26061.72559123 +.00000000 +00000-0 +00000-0 0 00007
2 27619 65.5028 319.3952 0011487 252.0405 275.6382 2.13103436 00
| Epoch (UTC): | 02 March 2026 17:24:51 |
| Eccentricity: | 0.0011487 |
| inclination: | 65.5028° |
| perigee height: | 19100 km |
| apogee height: | 19159 km |
| right ascension of ascending node: | 319.3952° |
| argument of perigee: | 252.0405° |
| revolutions per day: | 2.13103436 |
| mean anomaly at epoch: | 275.6382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|