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 26071.99280354 +.00000000 +00000-0 +87618-4 0 00008
2 16864 74.0287 306.4538 0032238 340.6056 19.3871 14.42276888 05
| Epoch (UTC): | 12 March 2026 23:49:38 |
| Eccentricity: | 0.0032238 |
| inclination: | 74.0287° |
| perigee height: | 728 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 306.4538° |
| argument of perigee: | 340.6056° |
| revolutions per day: | 14.42276888 |
| mean anomaly at epoch: | 19.3871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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