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 02653U 26130.98744458 +.00000000 +00000-0 +00000-0 0 00000
2 02653 8.1152 46.5859 0045328 61.8615 298.5107 1.07748358 06
| Epoch (UTC): | 10 May 2026 23:41:55 |
| Eccentricity: | 0.0045328 |
| inclination: | 8.1152° |
| perigee height: | 33631 km |
| apogee height: | 33995 km |
| right ascension of ascending node: | 46.5859° |
| argument of perigee: | 61.8615° |
| revolutions per day: | 1.07748358 |
| mean anomaly at epoch: | 298.5107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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