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 65245U 26145.56060479 +.00000000 +00000-0 +71262-4 0 00002
2 65245 97.4454 188.3361 0003117 116.4429 243.7118 15.05649738 00
| Epoch (UTC): | 25 May 2026 13:27:16 |
| Eccentricity: | 0.0003117 |
| inclination: | 97.4454° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 188.3361° |
| argument of perigee: | 116.4429° |
| revolutions per day: | 15.05649738 |
| mean anomaly at epoch: | 243.7118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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