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 65814U 26145.37370170 +.00000000 +00000-0 +41050-3 0 00006
2 65814 97.4532 8.2377 0001649 78.8317 281.3096 15.05657171 04
| Epoch (UTC): | 25 May 2026 08:58:07 |
| Eccentricity: | 0.0001649 |
| inclination: | 97.4532° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.2377° |
| argument of perigee: | 78.8317° |
| revolutions per day: | 15.05657171 |
| mean anomaly at epoch: | 281.3096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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