View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 02701U 65048E 22181.33149081 .00000186 00000-0 22354-3 0 9990
2 02701 89.9136 303.6124 0063275 205.7481 207.9179 13.62738475824068
| Epoch (UTC): | 30 June 2022 07:57:20 |
| Eccentricity: | 0.0063275 |
| inclination: | 89.9136° |
| perigee height: | 979 km |
| apogee height: | 1072 km |
| right ascension of ascending node: | 303.6124° |
| argument of perigee: | 205.7481° |
| revolutions per day: | 13.62738475 |
| mean anomaly at epoch: | 207.9179° |
| orbit number at epoch: | 82406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|