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 58997U 26145.62582602 +.00000000 +00000-0 +35339-3 0 00006
2 58997 97.6254 195.2566 0007440 47.1336 313.0503 14.84585625 09
| Epoch (UTC): | 25 May 2026 15:01:11 |
| Eccentricity: | 0.0007440 |
| inclination: | 97.6254° |
| perigee height: | 610 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 195.2566° |
| argument of perigee: | 47.1336° |
| revolutions per day: | 14.84585625 |
| mean anomaly at epoch: | 313.0503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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