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 28353U 26159.39300249 +.00000000 +00000-0 -93259-4 0 00000
2 28353 71.0021 42.1458 0007481 265.2419 94.7849 14.14612164 08
| Epoch (UTC): | 08 June 2026 09:25:55 |
| Eccentricity: | 0.0007481 |
| inclination: | 71.0021° |
| perigee height: | 838 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 42.1458° |
| argument of perigee: | 265.2419° |
| revolutions per day: | 14.14612164 |
| mean anomaly at epoch: | 94.7849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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