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 68121U 26145.34065681 +.00000000 +00000-0 +60721-3 0 00001
2 68121 97.2829 106.0218 0001955 92.0963 268.0503 15.33456458 02
| Epoch (UTC): | 25 May 2026 08:10:32 |
| Eccentricity: | 0.0001955 |
| inclination: | 97.2829° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 106.0218° |
| argument of perigee: | 92.0963° |
| revolutions per day: | 15.33456458 |
| mean anomaly at epoch: | 268.0503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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