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 48359U 26145.03144247 +.00000000 +00000-0 +20621-3 0 00009
2 48359 53.1603 3.4021 0001148 92.4788 267.6345 15.31722279 03
| Epoch (UTC): | 25 May 2026 00:45:16 |
| Eccentricity: | 0.0001148 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 3.4021° |
| argument of perigee: | 92.4788° |
| revolutions per day: | 15.31722279 |
| mean anomaly at epoch: | 267.6345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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