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 21047U 26103.41335793 +.00000000 +00000-0 +00000-0 0 00004
2 21047 13.0323 355.1584 0003984 253.2780 298.5986 0.98284820 08
| Epoch (UTC): | 13 April 2026 09:55:14 |
| Eccentricity: | 0.0003984 |
| inclination: | 13.0323° |
| perigee height: | 36336 km |
| apogee height: | 36370 km |
| right ascension of ascending node: | 355.1584° |
| argument of perigee: | 253.2780° |
| revolutions per day: | 0.98284820 |
| mean anomaly at epoch: | 298.5986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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