View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65299U 26145.14968494 +.00000000 +00000-0 +22180-3 0 00003
2 65299 97.9600 228.9077 0014753 155.1642 205.0283 14.80626166 03
| Epoch (UTC): | 25 May 2026 03:35:32 |
| Eccentricity: | 0.0014753 |
| inclination: | 97.9600° |
| perigee height: | 617 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 228.9077° |
| argument of perigee: | 155.1642° |
| revolutions per day: | 14.80626166 |
| mean anomaly at epoch: | 205.0283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|