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 28738U 26041.94189174 +.00000000 +00000-0 +50136-3 0 00005
2 28738 97.3619 56.1577 0007557 110.6705 249.5362 15.57783543 09
| Epoch (UTC): | 10 February 2026 22:36:19 |
| Eccentricity: | 0.0007557 |
| inclination: | 97.3619° |
| perigee height: | 389 km |
| apogee height: | 399 km |
| right ascension of ascending node: | 56.1577° |
| argument of perigee: | 110.6705° |
| revolutions per day: | 15.57783543 |
| mean anomaly at epoch: | 249.5362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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