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 60096U 26145.43709258 +.00000000 +00000-0 +43994-7 0 00006
2 60096 53.1619 40.8691 0001337 88.9982 271.1172 15.30188258 06
| Epoch (UTC): | 25 May 2026 10:29:24 |
| Eccentricity: | 0.0001337 |
| inclination: | 53.1619° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.8691° |
| argument of perigee: | 88.9982° |
| revolutions per day: | 15.30188258 |
| mean anomaly at epoch: | 271.1172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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