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 64240U 26145.24672200 +.00000000 +00000-0 +12924-2 0 00000
2 64240 43.0008 107.7861 0002061 263.5633 96.5000 15.70882849 02
| Epoch (UTC): | 25 May 2026 05:55:16 |
| Eccentricity: | 0.0002061 |
| inclination: | 43.0008° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 107.7861° |
| argument of perigee: | 263.5633° |
| revolutions per day: | 15.70882849 |
| mean anomaly at epoch: | 96.5000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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