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 60473U 26145.18340391 +.00000000 +00000-0 +40187-3 0 00003
2 60473 97.3777 228.3843 0001270 51.7092 308.4268 15.38926618 06
| Epoch (UTC): | 25 May 2026 04:24:06 |
| Eccentricity: | 0.0001270 |
| inclination: | 97.3777° |
| perigee height: | 448 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 228.3843° |
| argument of perigee: | 51.7092° |
| revolutions per day: | 15.38926618 |
| mean anomaly at epoch: | 308.4268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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