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 57971U 26145.36722735 +.00000000 +00000-0 +30045-3 0 00000
2 57971 42.9981 262.9275 0000754 275.3502 84.7264 15.27597505 04
| Epoch (UTC): | 25 May 2026 08:48:48 |
| Eccentricity: | 0.0000754 |
| inclination: | 42.9981° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 262.9275° |
| argument of perigee: | 275.3502° |
| revolutions per day: | 15.27597505 |
| mean anomaly at epoch: | 84.7264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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