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 63915U 26145.35515444 +.00000000 +00000-0 +35873-3 0 00005
2 63915 43.0004 103.1717 0001406 268.3465 91.7226 15.27588175 08
| Epoch (UTC): | 25 May 2026 08:31:25 |
| Eccentricity: | 0.0001406 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.1717° |
| argument of perigee: | 268.3465° |
| revolutions per day: | 15.27588175 |
| mean anomaly at epoch: | 91.7226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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