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 68370U 26145.43872987 +.00000000 +00000-0 +30933-3 0 00004
2 68370 82.2960 37.5143 0001017 256.2404 103.8753 15.87817909 00
| Epoch (UTC): | 25 May 2026 10:31:46 |
| Eccentricity: | 0.0001017 |
| inclination: | 82.2960° |
| perigee height: | 308 km |
| apogee height: | 309 km |
| right ascension of ascending node: | 37.5143° |
| argument of perigee: | 256.2404° |
| revolutions per day: | 15.87817909 |
| mean anomaly at epoch: | 103.8753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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