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 26067.29443131 +.00000000 +00000-0 +00000-0 0 00009
2 28477 47.4051 140.0883 7022844 91.9347 342.5505 2.23818990 01
| Epoch (UTC): | 08 March 2026 07:03:58 |
| Eccentricity: | 0.7022844 |
| inclination: | 47.4051° |
| perigee height: | 972 km |
| apogee height: | 35646 km |
| right ascension of ascending node: | 140.0883° |
| argument of perigee: | 91.9347° |
| revolutions per day: | 2.23818990 |
| mean anomaly at epoch: | 342.5505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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