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 28649U 26065.52691736 +.00000000 +00000-0 +20975-3 0 00006
2 28649 97.5415 93.2150 0002416 72.5351 287.6132 14.90752036 04
| Epoch (UTC): | 06 March 2026 12:38:45 |
| Eccentricity: | 0.0002416 |
| inclination: | 97.5415° |
| perigee height: | 594 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 93.2150° |
| argument of perigee: | 72.5351° |
| revolutions per day: | 14.90752036 |
| mean anomaly at epoch: | 287.6132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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