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 64843U 26145.10308145 +.00000000 +00000-0 +24707-3 0 00001
2 64843 97.4520 0.4259 0002203 82.8156 277.3322 15.05658805 00
| Epoch (UTC): | 25 May 2026 02:28:26 |
| Eccentricity: | 0.0002203 |
| inclination: | 97.4520° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.4259° |
| argument of perigee: | 82.8156° |
| revolutions per day: | 15.05658805 |
| mean anomaly at epoch: | 277.3322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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