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 28372U 26106.26487341 +.00000000 +00000-0 +50573-4 0 00009
2 28372 98.6332 115.2978 0044218 345.1229 14.8661 14.51744900 04
| Epoch (UTC): | 16 April 2026 06:21:25 |
| Eccentricity: | 0.0044218 |
| inclination: | 98.6332° |
| perigee height: | 689 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 115.2978° |
| argument of perigee: | 345.1229° |
| revolutions per day: | 14.51744900 |
| mean anomaly at epoch: | 14.8661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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