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 57444U 26145.45964042 +.00000000 +00000-0 +27785-4 0 00002
2 57444 43.0030 189.6219 0001508 261.4658 98.6023 15.27568669 01
| Epoch (UTC): | 25 May 2026 11:01:52 |
| Eccentricity: | 0.0001508 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.6219° |
| argument of perigee: | 261.4658° |
| revolutions per day: | 15.27568669 |
| mean anomaly at epoch: | 98.6023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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