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 53088U 26145.21565811 +.00000000 +00000-0 +56059-3 0 00002
2 53088 97.4449 325.0883 0001195 96.9423 263.1940 15.05609077 06
| Epoch (UTC): | 25 May 2026 05:10:32 |
| Eccentricity: | 0.0001195 |
| inclination: | 97.4449° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.0883° |
| argument of perigee: | 96.9423° |
| revolutions per day: | 15.05609077 |
| mean anomaly at epoch: | 263.1940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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