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 26134.95470785 +.00000000 +00000-0 +00000-0 0 00008
2 21047 13.0290 354.9789 0003557 240.2528 312.0069 0.98285406 02
| Epoch (UTC): | 14 May 2026 22:54:46 |
| Eccentricity: | 0.0003557 |
| inclination: | 13.0290° |
| perigee height: | 36338 km |
| apogee height: | 36368 km |
| right ascension of ascending node: | 354.9789° |
| argument of perigee: | 240.2528° |
| revolutions per day: | 0.98285406 |
| mean anomaly at epoch: | 312.0069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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