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 53450U 26145.47576865 +.00000000 +00000-0 +80724-3 0 00000
2 53450 97.5526 281.2611 0005101 251.7512 108.3211 15.99859327 08
| Epoch (UTC): | 25 May 2026 11:25:06 |
| Eccentricity: | 0.0005101 |
| inclination: | 97.5526° |
| perigee height: | 271 km |
| apogee height: | 278 km |
| right ascension of ascending node: | 281.2611° |
| argument of perigee: | 251.7512° |
| revolutions per day: | 15.99859327 |
| mean anomaly at epoch: | 108.3211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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