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 53082U 26145.22396189 +.00000000 +00000-0 +33258-3 0 00003
2 53082 97.4466 325.0918 0001094 70.8210 289.3136 15.05630934 04
| Epoch (UTC): | 25 May 2026 05:22:30 |
| Eccentricity: | 0.0001094 |
| inclination: | 97.4466° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.0918° |
| argument of perigee: | 70.8210° |
| revolutions per day: | 15.05630934 |
| mean anomaly at epoch: | 289.3136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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