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 68451U 26145.59104992 +.00000000 +00000-0 +33371-3 0 00004
2 68451 97.4490 104.3782 0003458 92.9545 267.2085 15.18530937 00
| Epoch (UTC): | 25 May 2026 14:11:06 |
| Eccentricity: | 0.0003458 |
| inclination: | 97.4490° |
| perigee height: | 508 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 104.3782° |
| argument of perigee: | 92.9545° |
| revolutions per day: | 15.18530937 |
| mean anomaly at epoch: | 267.2085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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