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 40045U 26156.40123382 +.00000000 +00000-0 +55761-3 0 00006
2 40045 97.7220 323.4766 0039364 56.6811 303.8171 14.97972844 03
| Epoch (UTC): | 05 June 2026 09:37:46 |
| Eccentricity: | 0.0039364 |
| inclination: | 97.7220° |
| perigee height: | 546 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 323.4766° |
| argument of perigee: | 56.6811° |
| revolutions per day: | 14.97972844 |
| mean anomaly at epoch: | 303.8171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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