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 53478U 26145.34441432 +.00000000 +00000-0 +74020-4 0 00000
2 53478 97.4485 265.2254 0000834 129.2358 230.8944 15.05649974 07
| Epoch (UTC): | 25 May 2026 08:15:57 |
| Eccentricity: | 0.0000834 |
| inclination: | 97.4485° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 265.2254° |
| argument of perigee: | 129.2358° |
| revolutions per day: | 15.05649974 |
| mean anomaly at epoch: | 230.8944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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