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 30209U 99025VS 22176.61356733 .00000330 00000-0 21118-3 0 9993
2 30209 98.7226 195.5432 0040775 232.3409 250.3736 14.09563184793506
| Epoch (UTC): | 25 June 2022 14:43:32 |
| Eccentricity: | 0.0040775 |
| inclination: | 98.7226° |
| perigee height: | 831 km |
| apogee height: | 890 km |
| right ascension of ascending node: | 195.5432° |
| argument of perigee: | 232.3409° |
| revolutions per day: | 14.09563184 |
| mean anomaly at epoch: | 250.3736° |
| orbit number at epoch: | 79350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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