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 60346U 26145.54511705 +.00000000 +00000-0 -33011-4 0 00001
2 60346 53.1603 78.5223 0001278 86.0540 274.0607 15.30200452 05
| Epoch (UTC): | 25 May 2026 13:04:58 |
| Eccentricity: | 0.0001278 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.5223° |
| argument of perigee: | 86.0540° |
| revolutions per day: | 15.30200452 |
| mean anomaly at epoch: | 274.0607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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