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 60402U 26145.51520472 +.00000000 +00000-0 +31032-4 0 00002
2 60402 53.1589 67.2187 0000950 81.2273 278.8852 15.69711801 02
| Epoch (UTC): | 25 May 2026 12:21:53 |
| Eccentricity: | 0.0000950 |
| inclination: | 53.1589° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 67.2187° |
| argument of perigee: | 81.2273° |
| revolutions per day: | 15.69711801 |
| mean anomaly at epoch: | 278.8852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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