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 47821U 26144.66761876 +.00000000 +00000-0 +30861-6 0 00003
2 47821 53.1576 249.5419 0001178 92.1590 267.9547 15.31694661 00
| Epoch (UTC): | 24 May 2026 16:01:22 |
| Eccentricity: | 0.0001178 |
| inclination: | 53.1576° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 249.5419° |
| argument of perigee: | 92.1590° |
| revolutions per day: | 15.31694661 |
| mean anomaly at epoch: | 267.9547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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