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 64103U 26145.40552911 +.00000000 +00000-0 +98320-3 0 00007
2 64103 53.1620 30.7368 0001299 91.6757 268.4393 15.30201500 08
| Epoch (UTC): | 25 May 2026 09:43:57 |
| Eccentricity: | 0.0001299 |
| inclination: | 53.1620° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.7368° |
| argument of perigee: | 91.6757° |
| revolutions per day: | 15.30201500 |
| mean anomaly at epoch: | 268.4393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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