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 46487U 26145.63366784 +.00000000 +00000-0 +57553-3 0 00001
2 46487 82.4958 0.6618 0020778 80.7782 279.5647 12.42871982 08
| Epoch (UTC): | 25 May 2026 15:12:28 |
| Eccentricity: | 0.0020778 |
| inclination: | 82.4958° |
| perigee height: | 1478 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 0.6618° |
| argument of perigee: | 80.7782° |
| revolutions per day: | 12.42871982 |
| mean anomaly at epoch: | 279.5647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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