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 40115U 26145.59464997 +.00000000 +00000-0 +92674-4 0 00007
2 40115 97.8569 220.7395 0002425 61.6201 298.5258 14.84977347 07
| Epoch (UTC): | 25 May 2026 14:16:17 |
| Eccentricity: | 0.0002425 |
| inclination: | 97.8569° |
| perigee height: | 612 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 220.7395° |
| argument of perigee: | 61.6201° |
| revolutions per day: | 14.84977347 |
| mean anomaly at epoch: | 298.5258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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