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 40101U 26145.81151867 +.00000000 +00000-0 +00000-0 0 00004
2 40101 9.1880 57.4904 0014455 333.3778 214.9536 0.98724358 02
| Epoch (UTC): | 25 May 2026 19:28:35 |
| Eccentricity: | 0.0014455 |
| inclination: | 9.1880° |
| perigee height: | 36164 km |
| apogee height: | 36288 km |
| right ascension of ascending node: | 57.4904° |
| argument of perigee: | 333.3778° |
| revolutions per day: | 0.98724358 |
| mean anomaly at epoch: | 214.9536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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