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 61723U 26145.50306310 +.00000000 +00000-0 +10545-4 0 00007
2 61723 53.1617 68.7359 0001288 86.1263 273.9885 15.30189101 08
| Epoch (UTC): | 25 May 2026 12:04:24 |
| Eccentricity: | 0.0001288 |
| inclination: | 53.1617° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 68.7359° |
| argument of perigee: | 86.1263° |
| revolutions per day: | 15.30189101 |
| mean anomaly at epoch: | 273.9885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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