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 28497U 26150.26184816 +.00000000 +00000-0 +18150-3 0 00001
2 28497 98.2554 36.8185 0001773 56.6900 303.4484 14.88077683 08
| Epoch (UTC): | 30 May 2026 06:17:03 |
| Eccentricity: | 0.0001773 |
| inclination: | 98.2554° |
| perigee height: | 603 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 36.8185° |
| argument of perigee: | 56.6900° |
| revolutions per day: | 14.88077683 |
| mean anomaly at epoch: | 303.4484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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