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 26121.93112359 +.00000000 +00000-0 +48459-3 0 00008
2 57203 97.5115 188.5467 0007084 234.7375 125.3204 15.30923464 00
| Epoch (UTC): | 01 May 2026 22:20:49 |
| Eccentricity: | 0.0007084 |
| inclination: | 97.5115° |
| perigee height: | 468 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 188.5467° |
| argument of perigee: | 234.7375° |
| revolutions per day: | 15.30923464 |
| mean anomaly at epoch: | 125.3204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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