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 64846U 26145.34676620 +.00000000 +00000-0 +36889-3 0 00000
2 64846 97.4491 0.6994 0002097 81.0189 279.1276 15.05658324 00
| Epoch (UTC): | 25 May 2026 08:19:20 |
| Eccentricity: | 0.0002097 |
| inclination: | 97.4491° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.6994° |
| argument of perigee: | 81.0189° |
| revolutions per day: | 15.05658324 |
| mean anomaly at epoch: | 279.1276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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