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 45603U 26145.61203252 +.00000000 +00000-0 +13566-3 0 00004
2 45603 97.5081 152.0023 0011017 358.8636 1.2567 15.11432033 06
| Epoch (UTC): | 25 May 2026 14:41:19 |
| Eccentricity: | 0.0011017 |
| inclination: | 97.5081° |
| perigee height: | 524 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 152.0023° |
| argument of perigee: | 358.8636° |
| revolutions per day: | 15.11432033 |
| mean anomaly at epoch: | 1.2567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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