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 22U 59009A 25198.69084528 .00009640 00000-0 41285-3 0 9996
2 22 50.2742 302.5640 0090609 225.0689 134.2893 15.19729104504280
| Epoch (UTC): | 17 July 2025 16:34:49 |
| Eccentricity: | 0.0090609 |
| inclination: | 50.2742° |
| perigee height: | 444 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 302.5640° |
| argument of perigee: | 225.0689° |
| revolutions per day: | 15.19729104 |
| mean anomaly at epoch: | 134.2893° |
| orbit number at epoch: | 50428 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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