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 57203U 26067.45992080 +.00000000 +00000-0 +80920-3 0 00000
2 57203 97.5195 133.4272 0009762 80.5451 279.6892 15.29444820 06
| Epoch (UTC): | 08 March 2026 11:02:17 |
| Eccentricity: | 0.0009762 |
| inclination: | 97.5195° |
| perigee height: | 471 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 133.4272° |
| argument of perigee: | 80.5451° |
| revolutions per day: | 15.29444820 |
| mean anomaly at epoch: | 279.6892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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