View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39151U 13018B 22176.82210314 .00000900 00000-0 12308-3 0 9997
2 39151 97.9920 282.4557 0015887 224.5162 135.4774 14.80956737494919
| Epoch (UTC): | 25 June 2022 19:43:49 |
| Eccentricity: | 0.0015887 |
| inclination: | 97.9920° |
| perigee height: | 615 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 282.4557° |
| argument of perigee: | 224.5162° |
| revolutions per day: | 14.80956737 |
| mean anomaly at epoch: | 135.4774° |
| orbit number at epoch: | 49491 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|