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 61600U 26145.40347749 +.00000000 +00000-0 -28748-3 0 00005
2 61600 87.8909 25.6183 0001063 95.1569 264.9680 13.11418443 01
| Epoch (UTC): | 25 May 2026 09:41:00 |
| Eccentricity: | 0.0001063 |
| inclination: | 87.8909° |
| perigee height: | 1217 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 25.6183° |
| argument of perigee: | 95.1569° |
| revolutions per day: | 13.11418443 |
| mean anomaly at epoch: | 264.9680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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