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 28057U 26106.62712740 +.00000000 +00000-0 +51640-4 0 00009
2 28057 98.7509 77.4562 0001142 42.6352 317.4922 14.36720625 07
| Epoch (UTC): | 16 April 2026 15:03:03 |
| Eccentricity: | 0.0001142 |
| inclination: | 98.7509° |
| perigee height: | 769 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 77.4562° |
| argument of perigee: | 42.6352° |
| revolutions per day: | 14.36720625 |
| mean anomaly at epoch: | 317.4922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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