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 48314U 26145.24033914 +.00000000 +00000-0 -13257-4 0 00000
2 48314 53.1613 94.8478 0001567 96.1617 263.9563 15.31699117 07
| Epoch (UTC): | 25 May 2026 05:46:05 |
| Eccentricity: | 0.0001567 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 94.8478° |
| argument of perigee: | 96.1617° |
| revolutions per day: | 15.31699117 |
| mean anomaly at epoch: | 263.9563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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