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 26075.78571314 +.00000000 +00000-0 +35797-3 0 00000
2 28647 56.9967 216.1174 0062769 32.8309 327.6620 15.42969466 06
| Epoch (UTC): | 16 March 2026 18:51:25 |
| Eccentricity: | 0.0062769 |
| inclination: | 56.9967° |
| perigee height: | 395 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 216.1174° |
| argument of perigee: | 32.8309° |
| revolutions per day: | 15.42969466 |
| mean anomaly at epoch: | 327.6620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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