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 68010U 26145.50689970 +.00000000 +00000-0 +46457-3 0 00009
2 68010 43.0036 334.9170 0000503 285.6706 74.4090 15.27594215 07
| Epoch (UTC): | 25 May 2026 12:09:56 |
| Eccentricity: | 0.0000503 |
| inclination: | 43.0036° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 334.9170° |
| argument of perigee: | 285.6706° |
| revolutions per day: | 15.27594215 |
| mean anomaly at epoch: | 74.4090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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