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 23533U 26146.13675240 +.00000000 +00000-0 +60410-4 0 00001
2 23533 98.8030 160.2859 0006160 207.6743 195.0111 14.17020544 05
| Epoch (UTC): | 26 May 2026 03:16:55 |
| Eccentricity: | 0.0006160 |
| inclination: | 98.8030° |
| perigee height: | 831 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 160.2859° |
| argument of perigee: | 207.6743° |
| revolutions per day: | 14.17020544 |
| mean anomaly at epoch: | 195.0111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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