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 61230U 26145.65141330 +.00000000 +00000-0 +49116-3 0 00000
2 61230 97.3560 225.1274 0008268 346.8944 13.2080 15.29317711 00
| Epoch (UTC): | 25 May 2026 15:38:02 |
| Eccentricity: | 0.0008268 |
| inclination: | 97.3560° |
| perigee height: | 472 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 225.1274° |
| argument of perigee: | 346.8944° |
| revolutions per day: | 15.29317711 |
| mean anomaly at epoch: | 13.2080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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