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 28545U 26072.85261683 +.00000000 +00000-0 +10023-2 0 00001
2 28545 6.9632 89.3174 7016117 91.0818 342.9261 2.61933978 09
| Epoch (UTC): | 13 March 2026 20:27:46 |
| Eccentricity: | 0.7016117 |
| inclination: | 6.9632° |
| perigee height: | 255 km |
| apogee height: | 31449 km |
| right ascension of ascending node: | 89.3174° |
| argument of perigee: | 91.0818° |
| revolutions per day: | 2.61933978 |
| mean anomaly at epoch: | 342.9261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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