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 64457U 26145.24673929 +.00000000 +00000-0 +61848-3 0 00009
2 64457 53.1599 92.2704 0001159 86.0876 274.0259 15.34404747 03
| Epoch (UTC): | 25 May 2026 05:55:18 |
| Eccentricity: | 0.0001159 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.2704° |
| argument of perigee: | 86.0876° |
| revolutions per day: | 15.34404747 |
| mean anomaly at epoch: | 274.0259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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