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 26066.01530806 +.00000000 +00000-0 +60724-3 0 00006
2 28738 97.3597 81.0635 0006290 53.4811 306.7024 15.59849903 07
| Epoch (UTC): | 07 March 2026 00:22:02 |
| Eccentricity: | 0.0006290 |
| inclination: | 97.3597° |
| perigee height: | 384 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 81.0635° |
| argument of perigee: | 53.4811° |
| revolutions per day: | 15.59849903 |
| mean anomaly at epoch: | 306.7024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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