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 28647U 26064.70527389 +.00000000 +00000-0 +48600-3 0 00000
2 28647 56.9962 263.7756 0061185 12.8078 347.4513 15.42488095 02
| Epoch (UTC): | 05 March 2026 16:55:35 |
| Eccentricity: | 0.0061185 |
| inclination: | 56.9962° |
| perigee height: | 397 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 263.7756° |
| argument of perigee: | 12.8078° |
| revolutions per day: | 15.42488095 |
| mean anomaly at epoch: | 347.4513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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