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 64624U 26145.43640100 +.00000000 +00000-0 +36845-3 0 00000
2 64624 97.4408 149.7913 0012719 196.0166 164.0670 15.22756042 07
| Epoch (UTC): | 25 May 2026 10:28:25 |
| Eccentricity: | 0.0012719 |
| inclination: | 97.4408° |
| perigee height: | 489 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 149.7913° |
| argument of perigee: | 196.0166° |
| revolutions per day: | 15.22756042 |
| mean anomaly at epoch: | 164.0670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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