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 57377U 26145.55481352 +.00000000 +00000-0 +77124-5 0 00009
2 57377 43.0021 170.2483 0001508 274.6124 85.4552 15.20040523 07
| Epoch (UTC): | 25 May 2026 13:18:55 |
| Eccentricity: | 0.0001508 |
| inclination: | 43.0021° |
| perigee height: | 505 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 170.2483° |
| argument of perigee: | 274.6124° |
| revolutions per day: | 15.20040523 |
| mean anomaly at epoch: | 85.4552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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