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 60403U 26145.51040639 +.00000000 +00000-0 +97286-5 0 00009
2 60403 53.1585 67.9187 0000872 87.1298 272.9820 15.69707138 09
| Epoch (UTC): | 25 May 2026 12:14:59 |
| Eccentricity: | 0.0000872 |
| inclination: | 53.1585° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 67.9187° |
| argument of perigee: | 87.1298° |
| revolutions per day: | 15.69707138 |
| mean anomaly at epoch: | 272.9820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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