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 48972U 26145.28309125 +.00000000 +00000-0 -85399-4 0 00000
2 48972 87.9108 233.3200 0001683 100.7867 259.3454 13.16593011 07
| Epoch (UTC): | 25 May 2026 06:47:39 |
| Eccentricity: | 0.0001683 |
| inclination: | 87.9108° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.3200° |
| argument of perigee: | 100.7867° |
| revolutions per day: | 13.16593011 |
| mean anomaly at epoch: | 259.3454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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