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 68112U 26145.62615105 +.00000000 +00000-0 +91924-3 0 00003
2 68112 97.2848 106.2469 0002228 94.4994 265.6504 15.33446386 00
| Epoch (UTC): | 25 May 2026 15:01:39 |
| Eccentricity: | 0.0002228 |
| inclination: | 97.2848° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 106.2469° |
| argument of perigee: | 94.4994° |
| revolutions per day: | 15.33446386 |
| mean anomaly at epoch: | 265.6504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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