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 63824U 26145.55043194 +.00000000 +00000-0 +34002-3 0 00007
2 63824 42.9992 98.1128 0001283 265.9480 94.1225 15.27603652 07
| Epoch (UTC): | 25 May 2026 13:12:37 |
| Eccentricity: | 0.0001283 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 98.1128° |
| argument of perigee: | 265.9480° |
| revolutions per day: | 15.27603652 |
| mean anomaly at epoch: | 94.1225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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