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 60432U 26145.20898816 +.00000000 +00000-0 +39057-4 0 00006
2 60432 53.1601 221.7772 0001118 84.4286 275.6843 15.30193209 02
| Epoch (UTC): | 25 May 2026 05:00:56 |
| Eccentricity: | 0.0001118 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 221.7772° |
| argument of perigee: | 84.4286° |
| revolutions per day: | 15.30193209 |
| mean anomaly at epoch: | 275.6843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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