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 68490U 26145.39174196 +.00000000 +00000-0 +17553-3 0 00002
2 68490 97.7601 103.9746 0004006 96.3547 263.8128 14.91213453 06
| Epoch (UTC): | 25 May 2026 09:24:06 |
| Eccentricity: | 0.0004006 |
| inclination: | 97.7601° |
| perigee height: | 591 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 103.9746° |
| argument of perigee: | 96.3547° |
| revolutions per day: | 14.91213453 |
| mean anomaly at epoch: | 263.8128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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