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 26150.45726653 +.00000000 +00000-0 +21319-3 0 00000
2 28376 98.3409 106.7653 0001475 70.7395 289.3965 14.61298560 01
| Epoch (UTC): | 30 May 2026 10:58:27 |
| Eccentricity: | 0.0001475 |
| inclination: | 98.3409° |
| perigee height: | 688 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 106.7653° |
| argument of perigee: | 70.7395° |
| revolutions per day: | 14.61298560 |
| mean anomaly at epoch: | 289.3965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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