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 is defined by the following mean orbital elements,
1 16987U 26022.07933580 +.00000000 +00000-0 +95540-4 0 00008
2 16987 82.5128 246.2464 0017259 349.7506 123.6565 14.85309445 06
| Epoch (UTC): | 22 January 2026 01:54:14 |
| Eccentricity: | 0.0017259 |
| inclination: | 82.5128° |
| perigee height: | 601 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 246.2464° |
| argument of perigee: | 349.7506° |
| revolutions per day: | 14.85309445 |
| mean anomaly at epoch: | 123.6565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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