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 61695U 26145.33892448 +.00000000 +00000-0 +76052-5 0 00004
2 61695 53.1604 8.3023 0001085 95.7272 264.3870 15.69703482 05
| Epoch (UTC): | 25 May 2026 08:08:03 |
| Eccentricity: | 0.0001085 |
| inclination: | 53.1604° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 8.3023° |
| argument of perigee: | 95.7272° |
| revolutions per day: | 15.69703482 |
| mean anomaly at epoch: | 264.3870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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