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 01864U 26088.17880479 +.00000000 +00000-0 +19398-3 0 00003
2 01864 89.0659 243.1969 0111733 97.2121 264.1764 13.79039724 05
| Epoch (UTC): | 29 March 2026 04:17:28 |
| Eccentricity: | 0.0111733 |
| inclination: | 89.0659° |
| perigee height: | 885 km |
| apogee height: | 1049 km |
| right ascension of ascending node: | 243.1969° |
| argument of perigee: | 97.2121° |
| revolutions per day: | 13.79039724 |
| mean anomaly at epoch: | 264.1764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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