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 68942U 26145.37977057 +.00000000 +00000-0 +40650-3 0 00003
2 68942 51.8766 177.6552 0004755 79.8501 280.3020 15.34356053 08
| Epoch (UTC): | 25 May 2026 09:06:52 |
| Eccentricity: | 0.0004755 |
| inclination: | 51.8766° |
| perigee height: | 460 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 177.6552° |
| argument of perigee: | 79.8501° |
| revolutions per day: | 15.34356053 |
| mean anomaly at epoch: | 280.3020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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