View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 37152U 10043A 24278.90663233 .00000058 00000-0 35044-3 0 9993
2 37152 82.4517 93.0303 0001745 69.7052 44.6115 12.42954492638449
| Epoch (UTC): | 04 October 2024 21:45:33 |
| Eccentricity: | 0.0001745 |
| inclination: | 82.4517° |
| perigee height: | 1493 km |
| apogee height: | 1495 km |
| right ascension of ascending node: | 93.0303° |
| argument of perigee: | 69.7052° |
| revolutions per day: | 12.42954492 |
| mean anomaly at epoch: | 44.6115° |
| orbit number at epoch: | 63844 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|