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 28376U 26145.59568056 +.00000000 +00000-0 +14269-3 0 00006
2 28376 98.3406 101.8646 0001544 71.6705 288.4664 14.61288137 03
| Epoch (UTC): | 25 May 2026 14:17:46 |
| Eccentricity: | 0.0001544 |
| inclination: | 98.3406° |
| perigee height: | 688 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 101.8646° |
| argument of perigee: | 71.6705° |
| revolutions per day: | 14.61288137 |
| mean anomaly at epoch: | 288.4664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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