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 18794U 26087.92892534 +.00000000 +00000-0 +10888-3 0 00005
2 18794 82.5970 73.1003 0036614 296.2896 89.4484 12.55585131 01
| Epoch (UTC): | 28 March 2026 22:17:39 |
| Eccentricity: | 0.0036614 |
| inclination: | 82.5970° |
| perigee height: | 1413 km |
| apogee height: | 1470 km |
| right ascension of ascending node: | 73.1003° |
| argument of perigee: | 296.2896° |
| revolutions per day: | 12.55585131 |
| mean anomaly at epoch: | 89.4484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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