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 68997U 26145.47042338 +.00000000 +00000-0 +15137-3 0 00001
2 68997 97.7387 43.3455 0001987 179.2772 180.8450 14.91770300 04
| Epoch (UTC): | 25 May 2026 11:17:24 |
| Eccentricity: | 0.0001987 |
| inclination: | 97.7387° |
| perigee height: | 591 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 43.3455° |
| argument of perigee: | 179.2772° |
| revolutions per day: | 14.91770300 |
| mean anomaly at epoch: | 180.8450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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