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 48772U 26145.38082102 +.00000000 +00000-0 +38814-3 0 00000
2 48772 87.9000 263.7304 0001862 94.4954 265.6389 13.15547382 09
| Epoch (UTC): | 25 May 2026 09:08:22 |
| Eccentricity: | 0.0001862 |
| inclination: | 87.9000° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7304° |
| argument of perigee: | 94.4954° |
| revolutions per day: | 13.15547382 |
| mean anomaly at epoch: | 265.6389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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