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 64954U 26145.12859553 +.00000000 +00000-0 +15130-3 0 00000
2 64954 97.4495 8.9911 0002293 78.6397 281.5088 15.05656188 09
| Epoch (UTC): | 25 May 2026 03:05:10 |
| Eccentricity: | 0.0002293 |
| inclination: | 97.4495° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.9911° |
| argument of perigee: | 78.6397° |
| revolutions per day: | 15.05656188 |
| mean anomaly at epoch: | 281.5088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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