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 61917U 26145.51893881 +.00000000 +00000-0 +90768-3 0 00001
2 61917 42.9993 207.7171 0001636 269.4501 90.6163 15.27596559 09
| Epoch (UTC): | 25 May 2026 12:27:16 |
| Eccentricity: | 0.0001636 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.7171° |
| argument of perigee: | 269.4501° |
| revolutions per day: | 15.27596559 |
| mean anomaly at epoch: | 90.6163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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