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 68994U 26145.66025556 +.00000000 +00000-0 +37842-3 0 00009
2 68994 97.7356 43.5540 0002597 63.4103 296.7382 14.92390990 09
| Epoch (UTC): | 25 May 2026 15:50:46 |
| Eccentricity: | 0.0002597 |
| inclination: | 97.7356° |
| perigee height: | 589 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 43.5540° |
| argument of perigee: | 63.4103° |
| revolutions per day: | 14.92390990 |
| mean anomaly at epoch: | 296.7382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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