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 28155U 26157.93947288 +.00000000 +00000-0 +99159-3 0 00001
2 28155 12.6615 258.6674 6194109 308.6237 10.6495 3.71089908 01
| Epoch (UTC): | 06 June 2026 22:32:50 |
| Eccentricity: | 0.6194109 |
| inclination: | 12.6615° |
| perigee height: | 329 km |
| apogee height: | 22161 km |
| right ascension of ascending node: | 258.6674° |
| argument of perigee: | 308.6237° |
| revolutions per day: | 3.71089908 |
| mean anomaly at epoch: | 10.6495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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