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 55373U 26145.54733435 +.00000000 +00000-0 +91494-4 0 00009
2 55373 43.0023 247.8087 0001956 277.9439 82.1190 15.27571673 00
| Epoch (UTC): | 25 May 2026 13:08:09 |
| Eccentricity: | 0.0001956 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.8087° |
| argument of perigee: | 277.9439° |
| revolutions per day: | 15.27571673 |
| mean anomaly at epoch: | 82.1190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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