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 68721U 26145.58335647 +.00000000 +00000-0 -45227-1 0 00008
2 68721 53.1610 36.8580 0001177 91.0916 11.0373 15.42902032 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.1610° |
| perigee height: | 437 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 36.8580° |
| argument of perigee: | 91.0916° |
| revolutions per day: | 15.42902032 |
| mean anomaly at epoch: | 11.0373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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