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 26076.10965265 +.00000000 +00000-0 +33278-3 0 00001
2 28647 56.9967 214.7234 0062736 33.4322 327.0669 15.42979327 07
| Epoch (UTC): | 17 March 2026 02:37:53 |
| Eccentricity: | 0.0062736 |
| inclination: | 56.9967° |
| perigee height: | 395 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 214.7234° |
| argument of perigee: | 33.4322° |
| revolutions per day: | 15.42979327 |
| mean anomaly at epoch: | 327.0669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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