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 65738U 26145.50905238 +.00000000 +00000-0 +57354-3 0 00009
2 65738 53.1600 336.1724 0001320 91.6945 268.4207 15.30205259 03
| Epoch (UTC): | 25 May 2026 12:13:02 |
| Eccentricity: | 0.0001320 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 336.1724° |
| argument of perigee: | 91.6945° |
| revolutions per day: | 15.30205259 |
| mean anomaly at epoch: | 268.4207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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