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 40376U 26072.01165003 +.00000000 +00000-0 +13674-3 0 00000
2 40376 98.1312 80.4538 0001505 110.5076 249.6288 14.63344081 08
| Epoch (UTC): | 13 March 2026 00:16:46 |
| Eccentricity: | 0.0001505 |
| inclination: | 98.1312° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 80.4538° |
| argument of perigee: | 110.5076° |
| revolutions per day: | 14.63344081 |
| mean anomaly at epoch: | 249.6288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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