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 60343U 26145.62098113 +.00000000 +00000-0 +24762-4 0 00002
2 60343 53.1609 78.2514 0001406 80.1564 279.9596 15.30193710 01
| Epoch (UTC): | 25 May 2026 14:54:12 |
| Eccentricity: | 0.0001406 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.2514° |
| argument of perigee: | 80.1564° |
| revolutions per day: | 15.30193710 |
| mean anomaly at epoch: | 279.9596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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