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 16987U 86074B 25188.12436922 .00000304 00000-0 32713-4 0 9996
2 16987 82.5149 73.2644 0016040 283.9006 188.9915 14.85057516 73516
| Epoch (UTC): | 07 July 2025 02:59:05 |
| Eccentricity: | 0.0016040 |
| inclination: | 82.5149° |
| perigee height: | 602 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 73.2644° |
| argument of perigee: | 283.9006° |
| revolutions per day: | 14.85057516 |
| mean anomaly at epoch: | 188.9915° |
| orbit number at epoch: | 7351 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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