View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 20625U 90046B 23154.56217472 -.00000124 00000-0 -39341-4 0 9996
2 20625 70.9988 258.8938 0012942 32.3094 327.8819 14.14750470705519
| Epoch (UTC): | 03 June 2023 13:29:31 |
| Eccentricity: | 0.0012942 |
| inclination: | 70.9988° |
| perigee height: | 834 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 258.8938° |
| argument of perigee: | 32.3094° |
| revolutions per day: | 14.14750470 |
| mean anomaly at epoch: | 327.8819° |
| orbit number at epoch: | 70551 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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