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 68238U 26145.58335647 +.00000000 +00000-0 -26672-3 0 00006
2 68238 53.1597 292.9961 0000920 63.7686 103.1911 15.35399983 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000920 |
| inclination: | 53.1597° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 292.9961° |
| argument of perigee: | 63.7686° |
| revolutions per day: | 15.35399983 |
| mean anomaly at epoch: | 103.1911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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