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 26040.36316095 +.00000000 +00000-0 +15540-3 0 00001
2 16864 74.0298 5.1340 0030959 47.3774 312.9985 14.42252644 09
| Epoch (UTC): | 09 February 2026 08:42:57 |
| Eccentricity: | 0.0030959 |
| inclination: | 74.0298° |
| perigee height: | 729 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 5.1340° |
| argument of perigee: | 47.3774° |
| revolutions per day: | 14.42252644 |
| mean anomaly at epoch: | 312.9985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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