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 63827U 26145.34542411 +.00000000 +00000-0 +31481-3 0 00001
2 63827 43.0011 100.0151 0001352 271.1273 88.9424 15.27584813 08
| Epoch (UTC): | 25 May 2026 08:17:24 |
| Eccentricity: | 0.0001352 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.0151° |
| argument of perigee: | 271.1273° |
| revolutions per day: | 15.27584813 |
| mean anomaly at epoch: | 88.9424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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