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 54851U 26145.12471935 +.00000000 +00000-0 +23070-4 0 00002
2 54851 43.0062 49.6395 0001246 289.5425 70.5292 15.27575522 00
| Epoch (UTC): | 25 May 2026 02:59:35 |
| Eccentricity: | 0.0001246 |
| inclination: | 43.0062° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.6395° |
| argument of perigee: | 289.5425° |
| revolutions per day: | 15.27575522 |
| mean anomaly at epoch: | 70.5292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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