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 35953U 26087.90314478 +.00000000 +00000-0 +91646-3 0 00006
2 35953 98.6493 78.8978 0004631 9.2374 57.0161 14.28470756 06
| Epoch (UTC): | 28 March 2026 21:40:31 |
| Eccentricity: | 0.0004631 |
| inclination: | 98.6493° |
| perigee height: | 794 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 78.8978° |
| argument of perigee: | 9.2374° |
| revolutions per day: | 14.28470756 |
| mean anomaly at epoch: | 57.0161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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