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 65817U 26145.49973154 +.00000000 +00000-0 +48276-4 0 00001
2 65817 86.4984 51.5185 0001374 65.3273 294.8004 13.24405839 00
| Epoch (UTC): | 25 May 2026 11:59:36 |
| Eccentricity: | 0.0001374 |
| inclination: | 86.4984° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 51.5185° |
| argument of perigee: | 65.3273° |
| revolutions per day: | 13.24405839 |
| mean anomaly at epoch: | 294.8004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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