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 46028U 26145.33243409 +.00000000 +00000-0 +17054-4 0 00000
2 46028 53.1593 130.7054 0001340 99.7198 260.3954 15.30191688 00
| Epoch (UTC): | 25 May 2026 07:58:42 |
| Eccentricity: | 0.0001340 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 130.7054° |
| argument of perigee: | 99.7198° |
| revolutions per day: | 15.30191688 |
| mean anomaly at epoch: | 260.3954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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