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 52900U 26121.84542354 +.00000000 +00000-0 +14056-3 0 00005
2 52900 98.2193 264.5792 0008021 162.1570 197.9914 14.61790348 01
| Epoch (UTC): | 01 May 2026 20:17:24 |
| Eccentricity: | 0.0008021 |
| inclination: | 98.2193° |
| perigee height: | 682 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 264.5792° |
| argument of perigee: | 162.1570° |
| revolutions per day: | 14.61790348 |
| mean anomaly at epoch: | 197.9914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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