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 60117U 26145.42099013 +.00000000 +00000-0 +16587-5 0 00006
2 60117 53.1589 203.0890 0001156 106.6330 253.4815 15.69697837 01
| Epoch (UTC): | 25 May 2026 10:06:13 |
| Eccentricity: | 0.0001156 |
| inclination: | 53.1589° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 203.0890° |
| argument of perigee: | 106.6330° |
| revolutions per day: | 15.69697837 |
| mean anomaly at epoch: | 253.4815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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