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 26064.84843669 +.00000000 +00000-0 +12693-3 0 00008
2 16864 74.0299 319.7090 0031949 355.4516 4.6345 14.42272187 02
| Epoch (UTC): | 05 March 2026 20:21:44 |
| Eccentricity: | 0.0031949 |
| inclination: | 74.0299° |
| perigee height: | 728 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 319.7090° |
| argument of perigee: | 355.4516° |
| revolutions per day: | 14.42272187 |
| mean anomaly at epoch: | 4.6345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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