View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29228U 06021A 23152.42355592 .00002245 00000-0 16565-3 0 9999
2 29228 69.9359 318.8213 0007511 251.9763 108.0581 15.04801548934846
| Epoch (UTC): | 01 June 2023 10:09:55 |
| Eccentricity: | 0.0007511 |
| inclination: | 69.9359° |
| perigee height: | 547 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 318.8213° |
| argument of perigee: | 251.9763° |
| revolutions per day: | 15.04801548 |
| mean anomaly at epoch: | 108.0581° |
| orbit number at epoch: | 93484 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|