▸Orbital parameters

Orbit class	SSO
Inclination	97.4585°
Eccentricity	0.0004280
Period	94.8 min
Apogee	510 km
Perigee	504 km
Mean motion	15.19754456 rev/day
RAAN	186.9249°
Arg of perigee	274.9367°
Mean anomaly	85.1379°
B*	3.4204e-4
Rev at epoch	2,676

▸Two-line element set (TLE)

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

1 67398U 26004AM 26187.94187477 .00007250 00000-0 34204-3 0 9996

2 67398 97.4585 186.9249 0004280 274.9367 85.1379 15.19754456 26765

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TOMORROW-S10",
  "OBJECT_ID": "2026-004AM",
  "EPOCH": "2026-07-06T22:36:17.98+00:00",
  "MEAN_MOTION": 15.19754456,
  "ECCENTRICITY": 0.000428,
  "INCLINATION": 97.4585,
  "RA_OF_ASC_NODE": 186.9249,
  "ARG_OF_PERICENTER": 274.9367,
  "MEAN_ANOMALY": 85.1379,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67398,
  "REV_AT_EPOCH": 2676,
  "BSTAR": 0.00034204,
  "MEAN_MOTION_DOT": 0.0000725,
  "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-S10
Operator	Tomorrow.io (The Tomorrow Companies Inc.)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jan 11, 2026HIGHvia 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/67398

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