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 48368U 26145.60598297 +.00000000 +00000-0 +49177-5 0 00009
2 48368 53.1607 350.5228 0001578 94.5647 265.5534 15.30188285 05
| Epoch (UTC): | 25 May 2026 14:32:36 |
| Eccentricity: | 0.0001578 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 350.5228° |
| argument of perigee: | 94.5647° |
| revolutions per day: | 15.30188285 |
| mean anomaly at epoch: | 265.5534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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