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 17912U 87038B 25188.93704554 .00000340 00000-0 36909-4 0 9995
2 17912 82.5015 167.2844 0017825 251.9952 107.9321 14.85055588 42908
| Epoch (UTC): | 07 July 2025 22:29:20 |
| Eccentricity: | 0.0017825 |
| inclination: | 82.5015° |
| perigee height: | 601 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 167.2844° |
| argument of perigee: | 251.9952° |
| revolutions per day: | 14.85055588 |
| mean anomaly at epoch: | 107.9321° |
| orbit number at epoch: | 4290 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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