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 48327U 26145.14551052 +.00000000 +00000-0 -35859-5 0 00004
2 48327 53.1614 105.5065 0001387 102.9625 257.1532 15.31693363 07
| Epoch (UTC): | 25 May 2026 03:29:32 |
| Eccentricity: | 0.0001387 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 105.5065° |
| argument of perigee: | 102.9625° |
| revolutions per day: | 15.31693363 |
| mean anomaly at epoch: | 257.1532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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