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 60437U 26145.46416348 +.00000000 +00000-0 +30193-4 0 00007
2 60437 53.1600 219.8160 0001031 86.0782 274.0339 15.34387821 00
| Epoch (UTC): | 25 May 2026 11:08:23 |
| Eccentricity: | 0.0001031 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.8160° |
| argument of perigee: | 86.0782° |
| revolutions per day: | 15.34387821 |
| mean anomaly at epoch: | 274.0339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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