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 57977U 26145.65005558 +.00000000 +00000-0 +30394-3 0 00002
2 57977 43.0011 276.0394 0001962 273.6137 86.4490 15.27606582 07
| Epoch (UTC): | 25 May 2026 15:36:04 |
| Eccentricity: | 0.0001962 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 276.0394° |
| argument of perigee: | 273.6137° |
| revolutions per day: | 15.27606582 |
| mean anomaly at epoch: | 86.4490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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