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 48388U 26145.29834639 +.00000000 +00000-0 +19083-3 0 00000
2 48388 53.1606 349.0191 0001194 82.2189 277.8948 15.31697710 01
| Epoch (UTC): | 25 May 2026 07:09:37 |
| Eccentricity: | 0.0001194 |
| inclination: | 53.1606° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 349.0191° |
| argument of perigee: | 82.2189° |
| revolutions per day: | 15.31697710 |
| mean anomaly at epoch: | 277.8948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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