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 26073.58144948 +.00000000 +00000-0 +18730-3 0 00005
2 28649 97.5411 100.9106 0002154 63.1911 296.9527 14.90785481 05
| Epoch (UTC): | 14 March 2026 13:57:17 |
| Eccentricity: | 0.0002154 |
| inclination: | 97.5411° |
| perigee height: | 594 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 100.9106° |
| argument of perigee: | 63.1911° |
| revolutions per day: | 14.90785481 |
| mean anomaly at epoch: | 296.9527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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