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 55303U 26145.41618358 +.00000000 +00000-0 +99282-4 0 00007
2 55303 69.9995 210.8008 0003348 267.3618 92.7158 14.98327793 00
| Epoch (UTC): | 25 May 2026 09:59:18 |
| Eccentricity: | 0.0003348 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 210.8008° |
| argument of perigee: | 267.3618° |
| revolutions per day: | 14.98327793 |
| mean anomaly at epoch: | 92.7158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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