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 61617U 26145.56536071 +.00000000 +00000-0 +30293-3 0 00005
2 61617 34.9911 340.0135 0004100 131.0712 229.0357 15.23035564 08
| Epoch (UTC): | 25 May 2026 13:34:07 |
| Eccentricity: | 0.0004100 |
| inclination: | 34.9911° |
| perigee height: | 494 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 340.0135° |
| argument of perigee: | 131.0712° |
| revolutions per day: | 15.23035564 |
| mean anomaly at epoch: | 229.0357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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