▸Orbital parameters

Orbit class	SSO
Inclination	97.3985°
Eccentricity	0.0006984
Period	94.6 min
Apogee	503 km
Perigee	493 km
Mean motion	15.22594841 rev/day
RAAN	80.2898°
Arg of perigee	73.2103°
Mean anomaly	286.9900°
B*	1.5487e-4
Rev at epoch	7,281

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 63225U 25052R 26187.68761990 .00003530 00000-0 15487-3 0 9991

2 63225 97.3985 80.2898 0006984 73.2103 286.9900 15.22594841 72812

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TOMORROW-S6",
  "OBJECT_ID": "2025-052R",
  "EPOCH": "2026-07-06T16:30:10.359+00:00",
  "MEAN_MOTION": 15.22594841,
  "ECCENTRICITY": 0.0006984,
  "INCLINATION": 97.3985,
  "RA_OF_ASC_NODE": 80.2898,
  "ARG_OF_PERICENTER": 73.2103,
  "MEAN_ANOMALY": 286.99,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63225,
  "REV_AT_EPOCH": 7281,
  "BSTAR": 0.00015487,
  "MEAN_MOTION_DOT": 0.0000353,
  "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-S6
Operator	Tomorrow.io (The Tomorrow Companies Inc.)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Mar 15, 2025HIGHvia 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/63225

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