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 68988U 26145.61993509 +.00000000 +00000-0 +10735-3 0 00001
2 68988 97.7367 43.4546 0005508 215.3918 144.6935 14.90565450 04
| Epoch (UTC): | 25 May 2026 14:52:42 |
| Eccentricity: | 0.0005508 |
| inclination: | 97.7367° |
| perigee height: | 592 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 43.4546° |
| argument of perigee: | 215.3918° |
| revolutions per day: | 14.90565450 |
| mean anomaly at epoch: | 144.6935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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