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 data is extracted from the following two-line orbital elements,
1 28353U 04021B 25107.81872910 -.00000143 00000-0 -49839-4 0 9996
2 28353 71.0018 196.3250 0005392 202.1158 157.9733 14.14540023 76758
| Epoch (UTC): | 17 April 2025 19:38:58 |
| Eccentricity: | 0.0005392 |
| inclination: | 71.0018° |
| perigee height: | 840 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 196.3250° |
| argument of perigee: | 202.1158° |
| revolutions per day: | 14.14540023 |
| mean anomaly at epoch: | 157.9733° |
| orbit number at epoch: | 7675 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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