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 28375U 26106.46771293 +.00000000 +00000-0 +51698-4 0 00005
2 28375 98.6564 69.3542 0079154 303.6652 55.7006 14.43844942 01
| Epoch (UTC): | 16 April 2026 11:13:30 |
| Eccentricity: | 0.0079154 |
| inclination: | 98.6564° |
| perigee height: | 689 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 69.3542° |
| argument of perigee: | 303.6652° |
| revolutions per day: | 14.43844942 |
| mean anomaly at epoch: | 55.7006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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