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 30561U 99025ALB 22183.85695485 .00000080 00000-0 69608-4 0 9997
2 30561 98.7637 206.2127 0063144 79.5600 95.3486 14.09005997792470
| Epoch (UTC): | 02 July 2022 20:34:00 |
| Eccentricity: | 0.0063144 |
| inclination: | 98.7637° |
| perigee height: | 817 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 206.2127° |
| argument of perigee: | 79.5600° |
| revolutions per day: | 14.09005997 |
| mean anomaly at epoch: | 95.3486° |
| orbit number at epoch: | 79247 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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