View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 33504U 26041.85044826 +.00000000 +00000-0 +25858-3 0 00009
2 33504 82.4316 303.7639 0008964 252.4952 107.5315 15.42605368 00
| Epoch (UTC): | 10 February 2026 20:24:38 |
| Eccentricity: | 0.0008964 |
| inclination: | 82.4316° |
| perigee height: | 432 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 303.7639° |
| argument of perigee: | 252.4952° |
| revolutions per day: | 15.42605368 |
| mean anomaly at epoch: | 107.5315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|