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 65254U 26145.37784182 +.00000000 +00000-0 +30030-3 0 00002
2 65254 97.4474 188.1207 0001348 99.9700 260.1680 15.05662580 07
| Epoch (UTC): | 25 May 2026 09:04:05 |
| Eccentricity: | 0.0001348 |
| inclination: | 97.4474° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 188.1207° |
| argument of perigee: | 99.9700° |
| revolutions per day: | 15.05662580 |
| mean anomaly at epoch: | 260.1680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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