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 35756U 26145.61711272 +.00000000 +00000-0 +00000-0 0 00004
2 35756 0.8545 270.3659 0003305 155.6861 195.4374 1.00269892 05
| Epoch (UTC): | 25 May 2026 14:48:38 |
| Eccentricity: | 0.0003305 |
| inclination: | 0.8545° |
| perigee height: | 35773 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 270.3659° |
| argument of perigee: | 155.6861° |
| revolutions per day: | 1.00269892 |
| mean anomaly at epoch: | 195.4374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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