View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 49419U 26145.26704973 +.00000000 +00000-0 +54034-4 0 00006
2 49419 53.2147 245.3501 0000923 56.2111 303.8969 15.08829913 05
| Epoch (UTC): | 25 May 2026 06:24:33 |
| Eccentricity: | 0.0000923 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 245.3501° |
| argument of perigee: | 56.2111° |
| revolutions per day: | 15.08829913 |
| mean anomaly at epoch: | 303.8969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|