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 63821U 26145.26076311 +.00000000 +00000-0 +25666-3 0 00005
2 63821 43.0026 100.2450 0001247 263.7042 96.3668 15.27582668 05
| Epoch (UTC): | 25 May 2026 06:15:29 |
| Eccentricity: | 0.0001247 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.2450° |
| argument of perigee: | 263.7042° |
| revolutions per day: | 15.27582668 |
| mean anomaly at epoch: | 96.3668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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