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 65819U 26145.48465613 +.00000000 +00000-0 +68115-4 0 00002
2 65819 86.4945 51.4137 0001411 66.2101 293.9181 13.24406007 01
| Epoch (UTC): | 25 May 2026 11:37:54 |
| Eccentricity: | 0.0001411 |
| inclination: | 86.4945° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 51.4137° |
| argument of perigee: | 66.2101° |
| revolutions per day: | 13.24406007 |
| mean anomaly at epoch: | 293.9181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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