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 26088.22326831 +.00000000 +00000-0 +70403-4 0 00003
2 16987 82.5184 184.0641 0018804 123.6076 299.8453 14.85389646 05
| Epoch (UTC): | 29 March 2026 05:21:30 |
| Eccentricity: | 0.0018804 |
| inclination: | 82.5184° |
| perigee height: | 599 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 184.0641° |
| argument of perigee: | 123.6076° |
| revolutions per day: | 14.85389646 |
| mean anomaly at epoch: | 299.8453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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