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 64115U 26145.38753777 +.00000000 +00000-0 +74544-3 0 00002
2 64115 53.1612 29.9181 0001435 94.8752 265.2413 15.32490089 09
| Epoch (UTC): | 25 May 2026 09:18:03 |
| Eccentricity: | 0.0001435 |
| inclination: | 53.1612° |
| perigee height: | 467 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 29.9181° |
| argument of perigee: | 94.8752° |
| revolutions per day: | 15.32490089 |
| mean anomaly at epoch: | 265.2413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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