▸Orbital parameters

Orbit class	LEO
Inclination	44.9998°
Eccentricity	0.0001459
Period	94.2 min
Apogee	479 km
Perigee	477 km
Mean motion	15.29354934 rev/day
RAAN	184.5232°
Arg of perigee	45.5132°
Mean anomaly	314.5871°
B*	1.9381e-4
Rev at epoch	8,599

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 62392U 24247R 26188.02847369 .00005325 00000-0 19381-3 0 9995

2 62392 44.9998 184.5232 0001459 45.5132 314.5871 15.29354934 85996

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TOMORROW-S3",
  "OBJECT_ID": "2024-247R",
  "EPOCH": "2026-07-07T00:41:00.127+00:00",
  "MEAN_MOTION": 15.29354934,
  "ECCENTRICITY": 0.0001459,
  "INCLINATION": 44.9998,
  "RA_OF_ASC_NODE": 184.5232,
  "ARG_OF_PERICENTER": 45.5132,
  "MEAN_ANOMALY": 314.5871,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62392,
  "REV_AT_EPOCH": 8599,
  "BSTAR": 0.00019381,
  "MEAN_MOTION_DOT": 0.00005325,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	TOMORROW-S3
Operator	Tomorrow.io (The Tomorrow Companies Inc.)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Dec 21, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	12HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/62392

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.