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 65821U 26145.46987454 +.00000000 +00000-0 +11189-3 0 00003
2 65821 86.4984 51.5026 0001682 81.8160 278.3165 13.24417530 05
| Epoch (UTC): | 25 May 2026 11:16:37 |
| Eccentricity: | 0.0001682 |
| inclination: | 86.4984° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 51.5026° |
| argument of perigee: | 81.8160° |
| revolutions per day: | 13.24417530 |
| mean anomaly at epoch: | 278.3165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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