View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 37654U 78026JR 24279.67061164 .00002843 00000-0 97705-3 0 9991
2 37654 98.6036 245.8240 0110197 359.6148 174.6763 14.33468800119584
| Epoch (UTC): | 05 October 2024 16:05:40 |
| Eccentricity: | 0.0110197 |
| inclination: | 98.6036° |
| perigee height: | 701 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 245.8240° |
| argument of perigee: | 359.6148° |
| revolutions per day: | 14.33468800 |
| mean anomaly at epoch: | 174.6763° |
| orbit number at epoch: | 11958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|