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 61680U 26145.54869230 +.00000000 +00000-0 +29457-4 0 00000
2 61680 53.1620 94.0333 0001273 88.5420 271.5727 15.31706997 01
| Epoch (UTC): | 25 May 2026 13:10:07 |
| Eccentricity: | 0.0001273 |
| inclination: | 53.1620° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 94.0333° |
| argument of perigee: | 88.5420° |
| revolutions per day: | 15.31706997 |
| mean anomaly at epoch: | 271.5727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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