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 28477U 26073.54877226 +.00000000 +00000-0 +00000-0 0 00000
2 28477 47.4086 138.6163 7024452 93.2992 342.0436 2.23818991 00
| Epoch (UTC): | 14 March 2026 13:10:13 |
| Eccentricity: | 0.7024452 |
| inclination: | 47.4086° |
| perigee height: | 968 km |
| apogee height: | 35650 km |
| right ascension of ascending node: | 138.6163° |
| argument of perigee: | 93.2992° |
| revolutions per day: | 2.23818991 |
| mean anomaly at epoch: | 342.0436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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