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 26070.85316537 +.00000000 +00000-0 +77893-4 0 00005
2 16987 82.5172 200.3877 0017534 178.8292 297.7336 14.85370261 06
| Epoch (UTC): | 11 March 2026 20:28:33 |
| Eccentricity: | 0.0017534 |
| inclination: | 82.5172° |
| perigee height: | 600 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 200.3877° |
| argument of perigee: | 178.8292° |
| revolutions per day: | 14.85370261 |
| mean anomaly at epoch: | 297.7336° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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