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 40057U 26135.25499791 +.00000000 +00000-0 +23499-3 0 00002
2 40057 98.2562 38.3948 0007996 27.4144 332.7497 14.97553162 06
| Epoch (UTC): | 15 May 2026 06:07:11 |
| Eccentricity: | 0.0007996 |
| inclination: | 98.2562° |
| perigee height: | 569 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 38.3948° |
| argument of perigee: | 27.4144° |
| revolutions per day: | 14.97553162 |
| mean anomaly at epoch: | 332.7497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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