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 16864U 26087.87682641 +.00000000 +00000-0 +75107-4 0 00007
2 16864 74.0264 276.9783 0032736 308.0458 51.7745 14.42283761 08
| Epoch (UTC): | 28 March 2026 21:02:37 |
| Eccentricity: | 0.0032736 |
| inclination: | 74.0264° |
| perigee height: | 728 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 276.9783° |
| argument of perigee: | 308.0458° |
| revolutions per day: | 14.42283761 |
| mean anomaly at epoch: | 51.7745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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