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 25509U 98061B 22222.07918567 .00000515 00000-0 86899-4 0 9993
2 25509 31.4322 199.1274 0345754 297.0992 59.4761 14.30675079243505
| Epoch (UTC): | 10 August 2022 01:54:01 |
| Eccentricity: | 0.0345754 |
| inclination: | 31.4322° |
| perigee height: | 541 km |
| apogee height: | 1037 km |
| right ascension of ascending node: | 199.1274° |
| argument of perigee: | 297.0992° |
| revolutions per day: | 14.30675079 |
| mean anomaly at epoch: | 59.4761° |
| orbit number at epoch: | 24350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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