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 57191U 26145.61300485 +.00000000 +00000-0 +20908-3 0 00003
2 57191 97.5063 203.5490 0015025 202.1601 157.8985 15.18860211 09
| Epoch (UTC): | 25 May 2026 14:42:43 |
| Eccentricity: | 0.0015025 |
| inclination: | 97.5063° |
| perigee height: | 499 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 203.5490° |
| argument of perigee: | 202.1601° |
| revolutions per day: | 15.18860211 |
| mean anomaly at epoch: | 157.8985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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